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The purpose of a power supply on a model railroad is to provide power to make the trains run, and if the layout is big enough and complex enough to require more than one power feed, the POLARITY is important. Otherwise, there will be short circuits, and the trains will not run. For the hundredth time, my layout is small enough and simple enough to run off of one DC power pack. Computerized Direct Digital Control would add complexity that I don’t need and expense that I cannot afford. Although my layout is big enough to give the illusion of visually separate scenes, I don’t have enough track space between the staging areas and the passing siding to allow more than one train in motion, so I simply alternate them. Besides, the tempo of operations on the single track Santa Fe line across northern New Mexico in the mid-1950’s was only five passenger trains and one through freight train a day each way plus a local freight that ran a few times a week.

 

I originally chose Kato Unitrack so I could quickly set up on my dinner table and run some trains and test various track arrangements without having to custom cut flex track and custom wire each track arrangement for my future layout. Once I built the layout, I have changed my passing sidings, industrial spurs, and staging yards several times by unsnapping, re-arranging, and popping the tracks back together. The Unitrack wiring system is simple “plug and play” with standard connectors and no soldering necessary.

 

When I first got started with Unitrack, I ordered a starter set that had an S-62F power feed track whose wiring cable ran to my Kato power pack. That worked fine for testing my brand new Super Chief in 2006. On longer track circuits the train ran slower further away from the power feed. I installed a second power feed track S-62F on the other side of the layout, and my train wouldn’t move. WTF? I checked for opens and found none, but the circuit breaker had popped. Both cables from the S-62F tracks connected to a 3 to 1 connector that snapped into the power pack. The connectors can only plug in the right way. Then I unplugged one of the power track feeds, and the train ran. I swapped power feeds, and the train ran but in the opposite direct. POLARITY PROBLEM! But how?

 

Most power feed tracks have big and unrealistic screw terminals for connecting both wires to the power pack. The sleek Kato S-62F track has a two wire cable that can run through a hole in the sub-roadbed or can be routed to an opening on either side of the track for temporary table top set-ups. These cable routing holes are near the end of the track, but the track can be snapped in either direction. When using only one S-62F power feed track, it doesn’t matter which direction the power feed track is placed in the small set-up, but if more than one is used, all the S-62F power feed holes must be oriented the same. I am not talking about whether the cables go left, right, or down but rather the location of the cable holes as you face the feeder track. Kato does not even mention it on the instructions that come with the track or in any of the booklets that come with track sets.

 

Here is how I standardize the polarity on my layout. Model manufactures for HO and N scales (and possibly others) have agreed that a POSITIVE voltage applied to the RIGHT rail and a NEGATIVE voltage to the LEFT will make an engine go FORWARD. Reversing circuits simply switch the polarity around to go backward. On many American layouts including mine, we arbitrarily decide that going RIGHT (as the viewer faces the layout) is EASTBOUND and going LEFT is WESTBOUND because many railfans in the Northern Hemisphere photograph east-west lines from the south side to allow the sun to illuminate the trains. I picked up that orientation when I was active in NTrak back in 1979-95. According to the General Code of Operating Rules followed by most American railroads, eastbound trains are superior to westbound trains of the same class. Therefore, the FORWARD setting on my Kato power pack is EASTBOUND, and the REVERSE setting is WESTBOUND. Given the fixed nature of the Kato Unitrack wiring plugs, in order to make the FORWARD setting propel the trains EASTBOUND, all the S-62F cable holes must be on the right as you face the track. I use two of these on my mainline and a third one on my portable test track. All of my staging tracks are reversing loops and powered by feeder UniJoiners which I’ll discuss later.

 

For clarity I unsnapped the feeder track from the track that holds an engine pointed Eastbound. Notice that the cable is on the RIGHT side as you view the track.

 

ROMA ARCHEOLOGICA & RESTAURO ARCHITETTURA: 'Roma - Una bellissima passeggiata nel Foro Romano, ricostruito in 3D.': Prof. Arch. Gilbert J. Gorski & Prof. James E. Packer, 'The Roman Forum: A Reconstruction and Architectural Guide', Cambridge University Press (2015 [Forthcoming]), pp. 1-474; 60 b/w illus. 247 colour illus. Foto: Cambridge University Press (05|2015).

 

"...Thus, while millions of casual tourists visit the site [of the Roman Forum] each year, most carry away only vague ideas of how the shattered ruins before them actually appeared in antiquity; and relevant literature in English usually provides little more." (...) "Since our new, restored model of the Forum is three dimensional, we were able to document the site in a realistic manner." (...) "With these digital materials and our texts, we anticipate that future visitors to the Forum will find the site more comprehensible – and, we hope, far more rewarding – than has ever previously been the case."

 

-- Prof. Arch. Gilbert J. Gorski & Prof. James E. Packer [2012-13] in: PREFACE, xv & xviii, Prof. Arch. Gilbert J. Gorski & Prof. James E. Packer, 'The Roman Forum: A Reconstruction and Architectural Guide', Cambridge University Press (2015 [Forthcoming]), pp. 1-474; 60 b/w illus. 247 colour illus.

 

The Roman Forum was in many ways the heart of the Roman Empire. Today, the Forum exists in a fragmentary state, having been destroyed and plundered by barbarians, aristocrats, citizens and priests over the past two millennia. Enough remains, however, for archaeologists to reconstruct its spectacular buildings and monuments. This richly illustrated volume provides an architectural history of the central section of the Roman Forum during the Empire (31 BCE–476 CE), from the Temple of Julius Caesar to the monuments on the slope of the Capitoline hill. Bringing together state-of-the-art technology in architectural illustration and the expertise of a prominent Roman archaeologist, this book offers a unique reconstruction of the Forum, providing architectural history, a summary of each building's excavation and research, scaled digital plans, elevations, and reconstructed aerial images that not only shed light on the Forum's history but vividly bring it to life. With this book, scholars, students, architects and artists will be able to visualize for the first time since antiquity the character, design and appearance of the famous heart of ancient Rome.

 

- With over 300 illustrations, the majority of them in color, this is the most complete and visually striking treatment of the Forum to date.

 

- Authored by an expert team of illustrator and Roman archaeologist.

 

- The reconstructions of every monument in the Forum constitute the handsomest, most complete, most attractive series of Forum images ever done.

 

Table of Contents

 

Part I. Architecture in the Roman Forum during the Empire: A Brief History:

1. The Augustan Reconstruction

2. From the Tiberius to Phocas (14–608 CE)

Part II. The Monuments:

3. The Temple of Antoninus and Faustina

4. The Temple of Caesar (Aedes divi Iuli)

5. The Basilica Aemilia

6. The Curia

7. The Arch of Septimius Severus

8. The West Rostra

9. The Temple of Concord

10. The Temple of Vespasian

11. The Tabularium

12. Portico of the Dei Consentes

13. The Temple of Saturn

14. The Basilica Julia

15. The Arch of Tiberius

16. The Schola Xanthi

17. The Diocletianic Honorary Columns

18. The Temple of Castor and Pollux

19. The Parthian Arch of Augustus

20. The Temple of Vesta

Part III. Conclusions.

 

Look Inside

 

- Index (PDF = 159 KB)

- Marketing Excerpt (PDF = 16615 KB)

- Copyright Information Page (PDF = 136 KB)

- Front Matter (PDF = 30244 KB)

- Table of Contents (PDF = 144 KB)

 

Authors

 

Gilbert J. Gorski, University of Notre Dame, Indiana -

 

Gilbert J. Gorski is a licensed architect and the project designer for numerous buildings including the World Headquarters for the McDonald's Corporation in Oak Brook, IL, and the Oceanarium, a major addition to the John G. Shedd Aquarium in Chicago. In 1987 he was designated the Burnham Fellow by the Chicago Architectural Club and was awarded an associate fellowship to the American Academy in Rome. Since 1989 Gorski has headed his own firm specializing in design and illustration. His drawings and paintings have been included in numerous publications and exhibits on architecture and illustration. He was twice awarded the Hugh Ferriss Memorial Prize, the nation's highest singular honor in architectural illustration, by the American Society of Architectural Illustrators. He is also the recipient of an Institute Honor for Collaborative Achievement, awarded by the American Institute of Architects. He presently is an associate professor at the University of Notre Dame and holds the James A. and Louise F. Nolen Chair in Architecture.

 

James E. Packer, Northwestern University, Illinois -

 

James E. Packer is Emeritus Professor of Classics at Northwestern University. He is the author of the three-volume The Forum of Trajan in Rome (1997); of numerous articles in journals, including the American Journal of Archaeology, the Journal of Roman Archaeology, the Bullettino della Commissione Archeologica Comunale di Roma, the Maryland Historian, Natural History, Croniche Pompeiane, Technology and Culture, Curator, Inland Architect, Archeo, and Archaeology; and of articles in collections, including the Lexicon Topographicum Urbis Romae (1993–2000). He is the recipient of many grants, including those from the Samuel H. Kress Foundation, the Getty Grant Program, the National Endowment for the Humanities, and the Andrew W. Mellon Foundation. He has excavated at Pompeii, in the Forum of Trajan (Rome), and in the Theater of Pompey (Rome). 'The Forum of Trajan' exhibition at the opening of the new Getty Museum in Los Angeles (1997) was based on Packer's work.

 

FOTO | TEXT | FONTE | SOURCE:

 

- Prof. Arch. Gilbert J. Gorski & Prof. James E. Packer, 'The Roman Forum: A Reconstruction and Architectural Guide', Cambridge University Press (2015 [Forthcoming]), pp. 1-474; 60 b/w illus. 247 colour illus.

 

www.cambridge.org/je/academic/subjects/archaeology/classi...

 

________________________________________________

 

s.v.,

 

-- ROMA ARCHEOLOGICA & RESTAURO ARCHITETTURA: “Un marmo sopra l’altro così rialzeremo le colonne del Foro di Traiano”, LA REPUBBLICA (15|04|2015). The Forum of Trajan, comments by prof. James E. Packer | FACEBOOK (15|04|2015).

 

wp.me/pPRv6-2Y1

 

________

 

“…Imperial Rome appears to be a golden, semi-mythical city filled with splendid monuments whose ruins still regularly attract hordes of annual visitors. Yet these tourists see only battered walls,fragmentary pavements, broken columns and piles of marble fragments mutely recalling past grandeur but giving little reliable information on the layout and visual or propagandistic effects of the originally elaborately decorated buildings. (…) Consequently, most visitors to Roman sites still rely either on simplified guide books or on ‘local’ professional guides who may or may not give their audience accurate (if limited and strictly verbal) information about the sites visited.”

 

Prof. James E. Packer, Digitalizing Roman Imperial architecture in the early 21st century: purposes, data, failures and prospects. JRAS 61 (2006), pg. 309 & 312 [of pages 309-320].

 

…His [Prof. Packer’s] interest in the monument [of the Forum of Trajan] was sparked in 1972,[1] while he was preparing to guide some Northwestern University [Illinois, USA] alumni on a tour of Rome, little had been published about the forum, he found. This did not surprise him. He had just finished his dissertation of the archaeological records of Ostia, the ancient port of Rome, and “it was extraordinary how much little had been done on Ostia,” [2] he says. “So it was not surprising that the same situation existed in Rome.” In fact, all of the Imperial Forums were “kind of forgotten” – collapsed, buried and hard to get into, he says.’ In a sense, Dr. Packer’s had been preparing for much of his life to play a role in the uncovering a key part of Roman history. “Ever since I was a child, I have been fascinated by Roman buildings,” he says. “I wanted to have something to do with them, but for a long time I wasn’t sure what.” As a boy, he made three-dimensional models of such buildings as the Forum of Pompeii, the Pantheon at Ostia, and the Round Temple of Baalbek in Lebanon. Growing up in Williamsburg, Virginia he was impressed by the town’s architecture. “My mother said, ‘if you like neo-classical architecture, wait until you see the real thing.’” Certainly the Forum of Trajan bore her out.’[2] & [4].

 

Notes: 1,2,3, & 4 in, see: ROMA ARCHEOLOGICA & RESTAURO ARCHITETTURA: Prof. James. E. Packer, (ed. it.), Il Foro di Traiano a Roma. Breve studio dei monumenti (Roma 2001). “[Prof. Packer] Passeggiata virtuale nel Foro Romano [e Traiano],” LA STAMPA (02|01|1998), p. 17.

 

wp.me/pPRv6-2Ut & www.flickr.com/photos/imperial_fora_of_rome/5189852726/

 

— ROME ARCHAEOLOGY & RESTAURO ARCHITETTURA: THE ROMAN FORUM – Prof. James E. Packer & Prof. Arch. Gilbert J. Gorski, “The Roman Forum: A Reconstruction and Architectural Guide,” Cambridge University Press (forthcoming [2014]), Pp. 550. Foto: Prof. James E. Packer, scholars and students visiting the Forum of Trajan in Oct. 2013.

 

wp.me/pPRv6-1Tz

 

— ROMA ARCHEOLOGIA e RESTAURO ARCHITETTURA: Prof. James E. Packer, Il Foro di Traiano. Breve studio dei monumenti | Prof. Packer, una lezione affascinante in inglese sul Foro di Traiano Roma (10|2013). [ENGLISH] VIDEO YOUTUBE [1:00:13].

 

wp.me/pPRv6-2pu

 

— ROMA ARCHEOLOGIA & RESTAURO ARCHITETTURA: Prof. James Packer,”Digitizing Imperial Rome: A computerized Approach to the Architectural History of the Roman Imperial Forum.” James Packer, Professor Emeritus Northwestern University (2010).

 

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— ROMA ARCHEOLOGICA & RESTAURO ARCHITETTURA: PROF. ANDREA CARANDINI, “IMAGO URBIS – Lazio , Roma e Suburbio,” LA SAPIENZA UNIVERSITA` DI ROMA | Arcus S.p.a | SSBAR (2015). Review of “ATLANTE DI ROMA ANTICA, Vol. I & II (2013),” by: T. P. Wiseman & J. E. Packer (2013).

 

wp.me/pPRv6-2NG

 

— ROMA ARCHEOLOGICA & RESTAURO ARCHITETTURA: Roma – I Fori Imperiali (1995-2008). The Forum of Trajan. Excavations & Related Studies (1998-2008). Prof. James. E. Packer, (ed. it.), Il Foro di Traiano a Roma. Breve studio dei monumenti (Roma 2001). [04|2008].

 

www.flickr.com/photos/imperial_fora_of_rome/2517676103/

 

— ROMA ARCHEOLOGIA e RESTUARO ARCHITETTURA: James E. Packer, Report from Rome: The Imperial Fora, a Retrospective [Relazione da Roma: I Fori Imperiali, una Retrospettiva]. AJA 101, April 1997, [PDF] 307-330. *

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______

 

Note: A very special thank you to both Prof. James E. Packer and Prof. Arch. Kevin Sarring, they were kind enough to meet with me here in Washington DC in late October 2009, prof. Packer more then generously shared with me the outline of his preliminary work for the current book: ‘The Roman Forum: A Reconstruction and Architectural Guide (2015); M. G. Conde [05|2015]

______

We are your ancient family. We come from the star system The Pleiades. We know ourselves as The Pleiadians and we, eons ago, millions of years ago, were your relatives.

 

When your Earth sphere, Terra, was being formed, there were many who expressed an interest to be pioneers and to go to a new area to learn to experience, to formulate, to create. That was the opportunity and many of our dearly beloved Pleiadians signed on.

 

The Pleiadian culture is ancient. [It] was seeded from another universe, a universe of love, a universe that moved back to All That Is. The Pleiadians seeded the Pleiadian star system within this universe before the Earth’s sphere transfer became available. We formed a tremendous society. We operate with love. We operate with ideas and ideals that you are totally unfamiliar with.

 

Our technology in your terms would be somewhat similar. We are, in your terms, computerized. We like that term because it represents an overall picture of our abilities. The picture actually only represents one per cent of what we are capable of doing. However, from your point of view, think of us as a computerized society. We are collective energy. We are not of your dimension.

 

The star system of the Pleiades has seven stars, six of which we believe, you may see from the naked eye. There are many planets and we are millions upon millions of miles from your system though we have transportation that can bring us here very quickly. We have many modes of transportation.

 

Mostly we come in starships. Often mother ships. The mother ships are gigantic, one of your miles, housing thousands. [They are] elongated, one of our fashions, [and] would take, in your terms, days to transport itself here. We have disc ships which can be here quickly, within portions of your day.

 

We have difficulty at times translating your time system, your hours, your minutes, into what is relative to our system, perhaps less than one quarter of your day. We are an advanced civilization. Our technology is ancient because it is coming from another universe that has evolved back to First Cause.

 

We chose not to evolve back to First Cause but to go on out of love, to assist the growth of this universe. We were allowed to bring that knowing with us because our technological development is totally in line with the First Cause and we would never operate in any fashion that did not support the love and development of humanity of all creatures in all of this universe. So we were allowed to be here. We were welcomed.

 

We are the ambassadors, in this star area, this universe, from another universe. We are working with many, not just with Terra, the Earth. We are working in other solar systems, with other planetary creatures, with other creations.

 

This universe is a vast and new experiment. Different options, we like that word, are being attempted here. Free will reigns in this universe. On Terra you think you have free will but you do not really understand what free will is. Free will encompasses the complete idea that whatever it is that you are wanting you may have. And your sole point in choosing to partake in the planetary system within this universe that has free will was so that you may do whatever it is that you wish.

 

Terra was formed with specific intents in mind. It was formed to be a center for this solar system, a trade center, a launching pad for ideas. Much like, as different portions of your globe have developed, and different port cities, or areas came into fashion and represented trends, cultural advancements, exchanges of ideas at different points in time, and then fell by the wayside.

 

The ideal of Terra’s role would be the jewel within the universe for its beauty physically to the eye, and this physical beauty would be beheld not just in one dimension but in many dimensions. That it would be a center of tremendous beauty, of tremendous exchange, of freedom, of ideas and beauty and love and peoples, humanities, creatures from all of this universe and star system ideally would have come here and exchanged what it is they had, as goods would be exchanged in the marketplace, with others.

 

Now, as you know, that has not taken place. Fortunately that is changing. Unfortunately, eons in your past, events occurred that were not anticipated, for when one deals with free will one never knows. There are no expectations with free will, just intentions and hopes. And even intentions sometimes may be transmuted.

 

Now, that was the original intention. Then eons ago, millions of years ago, there was a disruptive force that became quite pronounced in this area of creation, experimenting as it would be, with another form of being. This experimenting was not evil, it was just another point of view. We speak in very neutral terms so as not to lay blame or prejudice on anyone.

 

This disruptive force effected Terra greatly. It threw the cosmic forces, the hierarchies into vast confusion. And it has been all these eons, these millions of years that this has been attempted to be righted.

 

Now, through the last thousands of years we have been assisting the higher spiritual forces, those from the First Cause. Our assistance we freely gave because original family members came to this experiment of Terra and then when those disruptive energies became prevalent and changed the intent of what Terra would be we lost contact with our family members. It was very sad for us, for we had never anticipated this loss.

 

Being that we as Pleiadians are highly evolved and of great knowing and great connectedness with the First Cause, we knew that this was a temporary loss of family members, though temporary in our terms was millions of years. And though the initial shock was felt literally throughout the universe and universes, we formulated a plan and knew that there would be a time when we would be reunited.

 

We are your family members who lost contact with you eons ago. We have come to retrieve you. We have come to reestablish contact, to assist you, so that you can now reunite with us, liberate yourselves and choose to come back to the Pleiades or to stay here on Terra and raise the vibration and allow Terra to become what it was originally planned to become, the international exchange, intergalactic international trade exchange center for the universe.

 

Now, as you may well know, that upon looking at your planet you can shake your head and say, goodness, we have ventured far from our original goal. And, indeed, that is true, you have. However, at this time events are manifesting on your planet that are about to change all of that.

 

It was known eons ago that there would be a point where the energies would be ripe for contact, for adjustments, for receiving energy for realignment. It was hoped that that juncture would be reached through the opening of the free will bodies, by their own choice, through love.

 

That is not the case. You have reached critical times. It began peaking 30, 40 years ago, and the activities that have been occurring on this sphere have been of grave concern to all within your universe. The lack of love for humanity, for one another on this planet. Separations of self from self. The missing of the message that you are all one, that you are all connected, that what one does affects the other.

 

Know that there are many millions on the planet out of the billions, who are awakened, who are moving toward the enlightenment, moving towards the acknowledgement of the First Creator, in whatever minuscule way they can conceive of this vast entity.

 

What is happening on your planet at this time is that the energy of the First Creator, is being presented to the planet as a whole. When we say “as a whole”, there are no groupings that would be select over others. The opportunities exist for everyone. It is the individual humanity’s choice to acknowledge the opportunity that presents itself.

 

[The awakened ones will be] assigned, so to speak, to awaken someone. First Creator energy is now being made available to the planet, on a vast level, vast. It’s encircling the sphere. Light frequency is bombarding your planet, though only those who know how to use this energy can feel it. It is as if an invisible force is in your lives and if you are not aware of this invisible force, you will not see it.

 

Now, if the awakeners approach the awakenees with love, with intent of service, with intent of changing the planetary potential, the planetary history, and also are willing to bond unconditionally with the awakenee, it will be successful. In most cases, those that need now to be awakened are working about this in their dream state and they are in a state of confusion in their waking world and so they are welcoming something that will give them greater power and direction.

 

The awakenees will need guidance for a short amount of time because of the energy that is available [but] the knowings will happen very quickly, then they, too, [will awaken and empower others]. The more members, the greater members of humanity that are in knowing, the easier the times ahead will be.

 

We are working, sitting at the edges of our seats. When we say “our”, we mean our beings, the star individuals, the star families, the spirit guides, the ascended masters, the callers from the great cause, the First Cause. There are many here. The skies, the atmospheres are full, so to speak, of who we are keeping Terra in force, keeping it alive and vibrant, glowing, and also respecting your free will at the same time.

 

That is why we say the awakenings are so important at this time. They are of prime concern. Individual awakenings. Word of mouth. It is the best way of accomplishing what it is that needs to be accomplished. Word of mouth. Books are fine. Tapings are fine. But one individual loving another individual liberates, frees. And that individual goes off and creates and effects many others. That is how the process will occur, as we see it.

 

We stated earlier that Terra is a free will district along with the entire universe, however, there is a code of honor that exists along with free will. And that code of honor represents the respect for life. All of life. The respect, and the commitment to no violation of life. The honoring of life is paramount, and allowing that life.

 

Now, millions upon millions of years ago when the disruptive forces came in and changed all of that, free will was granted still and we stepped back, and saw and watched, and knew that there would be a time when all of this would come to an apex, as it would be said when the changes could be made.

 

Disruptive forces have come again. This time they will not succeed. However, the energy is of great influence on the planet at this time because of the technological development and the extent of this technological influence throughout the planet.

 

We ask that each person individually speak to another. At this point very powerful individuals are being awakened. Those individuals who effect other people, who influence other people are those that are awakening at this time, and are being awakened by those who made agreements, contracts eons ago to perform this service. We see that there will be changes geographically, great changes. Because the changes represent the most benevolent way of realignment. If there were to be great destructions, and there will be some destructions along the lines of warrings, if that were to be the prevalent case upon the entire sphere, it would effect the cosmos so greatly, that in this case it cannot be allowed.

 

The changes that will happen on the surface of Terra are not definite. They will not be definite until they occur, until energy peaks. The energy will be peaking partially through what’s happening on the globe, also through planetary and cosmic influences. The closer you may move towards the misuse of the technology, then of course, Mother Earth, a living, viable, breathing entity, would shift itself rather than destroy itself.

 

[The] shifts will be of a healing nature, much as the ill person may experience the tremendous fevers and burn and sweat and shake and then heal themselves. If Mother Earth did not shift herself and the misuse of technology would be [a] prevalent paradigm, do you know what would occur? It would be the destruction of the universe.

 

We do not wish to be annihilated and misuse of your technology on your planet could annihilate a universe. Contemplate on what we are speaking for it is profound.

 

Many of you are looking for blacks and whites and the universe exists in gray areas. It is not the way you think it is. There is life teeming everywhere that you cannot see. There are many dimensions, there are many forms of beings. What happens in your dimension would affect us all because the building blocks of the universe, of the cosmos are connected. The atoms, the elements are all one. They are universal. Universal tools, so to speak. And through the misuse of one, in one segmented area, it would effect many others. So that is why we say, we are tuning Mother Earth to this knowing. Mother Earth knows this potential happening and would shift herself when the time and the danger becomes great.

 

Understand that all of these changes are contingent upon the awakenings. If the awakenings happen very quickly and those within the governments, within the arms industries, those within the publishing, communicative areas, television, newspaper, movies, [if] those influential people on the planet are awakened quickly, all could shift. Mother Earth will do whatever is necessary to realign for her own survival.

 

We are saying that if your intention is to step into the times ahead with joy, and experience, and be a partaker, a conscious partaker of the movement that the planet is selecting, then clearly think of what it is that you want, intend it, plan on it, and then trust that the part of the body located in the solar plexus will guide you along with the heart, to be where it is you need to be. If you are clear in your plannings, if you count on it, if you state it matter of factly, step into the knowing, not the thinking, but the knowing beyond all shadow of a doubt that you will be here in joy, in harmony, in happiness, in creativity, and in greater rejoicing of building the world, the civilization that you all desire, then so shall you be.

 

Now, think of that for a few moments and choose what it is you want. Examine your hearts about what it is you are wanting. Throw by the wayside those things that are not important to you and put your energy, your thoughts, your hearts, into what it is that is most important. And do not, under any circumstances, be afraid of making a change, for change is going to occur whether you select it or not. So, by consciously selecting a change, whether it be a move, or what have you, [it] may be your method, your means, of moving into the times ahead.

 

Do not resist change. Flow. It may come in the area of relationships, the breakings up or the coming togethers. It may come in the area of employment or a lack of. It may come in the area of sudden abundance presenting itself to you or lack of. All these events will motivate you towards something. We ask that you go inside, trust the feelings. Trust yourself. One of the most beneficial endeavors that you will be involved with is forming the extended families. With a networking of thirty to fifty people it will be very powerful. We also wish to speak of the availability of outside communication that is waiting to speak with many of you, that is speaking with each and every one of you though you do not acknowledge it. Vast numbers are willing to help.

 

We ask you to examine your hearts, relinquish your fears, move towards what it is that will be most important. We suggest, and we will assist in these endeavors, that through your dream states you dare to dream of possibilities that seem outlandish. Awakened ones and those becoming awakened are being fed information through the dream state from the vast numbers and given so called ideas. Instigated information. Potentialities of abilities that are far beyond what is available now on the planet. And these will be fun things. These will be joyful things. These will be loving things, healing things, successful things. Play with your dream states and when one of these crazy ideas comes to you, grasp onto it like a hot air balloon and ride it for a while over the topography of yourself and see where it will take you.

 

We ask you to approach these times with an open mind, a creative mind, a loving mind, to move into the self. To trust the self. Open the heart. To connect with humanity, to awaken the others. To be gentle with who you are. For your difficulties you will lay down as they are old clothes that you will no longer fit into or wear. Your aches, longings and difficulties can all be laid to rest as you move into this great new garment of being.

 

Many will be petrified of moving into this time for much must be relinquished. Much must be changed and given up. However, we are saying that if the Earth itself did not change in its seasons, it would be pretty dreary indeed. And so fall needs to come and the winter set to rest so that in spring there may be regrowth, revitalization and awakenings. This is what you’ll be experiencing.

 

We have committed to guide you on this time. There are many who are here loving you, assisting you, doing whatever is necessary. Open your hearts. Open your eyes to what is coming. Do not be afraid. Know that you are surrounded by love and energy greater than at this point you can fathom. So great it is beyond your knowing, though a part of you knows that greatness and brings it to yourself.

 

We trust that what we have said empowers you, enlightens you, guides you to who you need to be. Move forward. Move in love. Feel the connectedness of all that is.

 

Look into the eyes of fellow humanity and see yourselves for you are there. Bless each one with the knowing that you have and your awakenings will be greater than you ever imagined.

 

goldenageofgaia.com/disclosure/who-are-the-extraterrestri...

RF-84F Thunderflash is the reconnaissance version of Republic F-84F Thunderstreak. The main difference, inherited from the second YF-84F prototype, were the wing-root air intakes. These were not adopted for the fighter version due to loss of thrust. However, this arrangement permitted placement of cameras in the nose and the design was adopted for the The aircraft retained an armament of four machine guns and could carry up to fifteen cameras. Innovations included computerized controls which adjusted camera settings for light, speed, and altitude, a periscope to give the pilot better visualization of the target, and a voice recorder to let the pilot narrate his observations.

 

West German Air Force ordered 108 RF-4F aircrafts out of 715 totally built. They served in Aufklärungsgeschwader 51 (Reconnaissance Wing) and Aufklärungsgeschwader 52. In June 1965 West German Air Force began to replace Thunderflashes with RF-104G Starfighter reconnaissance version starting with AG51. On August 31th 1966 the very last RF-84F retired the Luftwaffe.

 

This particular Republic RF-84F-25-RE from West German Air Force with registration EB-344 served with the USAF 66th TRW at Sembach prior to be transferred to Luftwaffe with AG52. Now it is preserved at "Luftwaffenmuseum der Bundeswehr Berlin-Gatow".

 

Construction Number (C/N): 52-7346. Probably wears fake EB-344 markings.

Westland Sea King HAR3 XZ594 (cn WA860) Royal Air Force, Sea King Rescue Training Unit (SKTU), on the Thursday before RIAT 2015 at Fairford UK (FFD). (photo 4829-1).

 

The Westland WS-61 Sea King is a British license-built version of the American Sikorsky S-61 helicopter of the same name, built by Westland Helicopters. The aircraft differs considerably from the American version, with Rolls-Royce Gnome engines (derived from the US General Electric T58), British-made anti-submarine warfare systems and a fully computerized flight control system.

 

A dedicated search and rescue (SAR) version, the HAR3, was developed for the RAF Search and Rescue Force. The type entered service in 1978. Westland also manufactured SAR versions of the Sea King for the Royal Norwegian Air Force, the German Navy and the Belgian Air Force. On SAR variants, the cabin was enlarged by a stretch of the fuselage behind the door; another key feature, used for additional flotation in the unusual event of a water landing, inflatable buoyancy bags were housed inside the aircraft's sponsons. Upgrades and changes made to SAR Sea Kings include the addition of radar warning receivers, a cargo hook for the underslung carriage of goods, and the redesigning of the cockpit for compatibility with night vision goggles. As of 2006, up to 12 HAR3/3As were dispersed across the UK, a further two HAR3s were attached to the Falkland Islands, providing 24-hour rescue coverage.

 

Source: en.wikipedia.org/wiki/Westland_Sea_King

+++ DISCLAIMER +++

Nothing you see here is real, even though the conversion or the presented background story might be based historical facts. BEWARE!

  

Some Background:

On 23 January 1992, the Lithuanian Minister of Defense signed an order establishing the staff for the Aviation Base of the Aviation Service. But an actual base in the Šiauliai airport territory (Barysiai airfield) was not established until March, when according to the ordinance of the Government of Lithuanian Republic, all the infrastructure, buildings, territory and 24 An-2 aircraft were passed from ”Lithuanian Airlines" to the Aviation Service of the Ministry of Defense in January 1992.

 

On 12 June 1992, the first time after regaining the independence of Lithuania, An-2 aircraft, marked with the double cross of Vytis on its wings – the distinguishing sign of Lithuanian Air Force – took off from Barysiai airfield. This date is considered to be the Aviation Base foundation date. In February 1993 four L-39C Albatros aircraft were brought from Kyrgyzstan.

 

After 1 March 1993 Aviation Service was reformed to the Lithuanian Air Force and Aviation Base was renamed the First Aviation Base of the Lithuanian Air Force. In January 1994 Lithuania officially applied for NATO membership, and the country also looked out for a relatively cheap multi-purpose fighter that would fulfill both air space defence and attack tasks, the latter primarily against potential targets at sea (e. g. fast hoovercraft landing ships operated by the Russian Baltic Fleet).

 

After evaluating several options, the Lithuanian Air Force settled for a surprising aircraft: the venerable MiG-21! After the demise of the Soviet Union, several international companies started to offer conversion and upgrade programs for the widely used tactical fighter, about 5.000 specimen had been built to date. One of the first companies to enter the market was Israel Aircraft Industries: IAI's Lahav Division of (IAI) had developed the so-called MiG-21 2000 upgraded fighter and ground attack version, based on the MiG-21bis and the export MiG-21MF fighter aircraft.

 

The MiG-21 2000 upgrade provided modifications to the cockpit configuration, avionics architecture and weapons systems, enabling the MiG-21 2000 to compete with Western developed fighters like the F-16 and to make the transition to Western standards. The aircraft's original systems and components were retained wherever mission effectiveness was not compromised.

IAI Lahav augmented the original weapons system by introducing an EL/M-2032 radar, developed by IAI Elta Electronic Industries, based in Ashdod. The radar, which uses a low sidelobe planar array antenna and pulse Doppler beam sharpening, provides all-altitude, all-aspect look-up / look-down and shoot-down capability, as well as beyond-visual-range capability. In order to make the radar compatible with Western ordnance, a new armament interface and control unit were added, too, which enabled computerized control and release of weapons, including third and fourth-generation air-to-air missiles and precision-guided munitions of Western and Eastern provenance.

 

This system also gave the pilot the ability to use blind attack as well as continuously computed impact point (CCIP) and dive-toss bombing techniques. CCIP bombing involves the deployment of air-to-ground weapons, using the HUD to indicate the impact point for release of the weapons. Dive-toss bombing involves the release of air-to-ground weapons at the end of a steep dive manoeuver towards the target.

 

The MiG-21 2000 cockpit featured a new pilot-friendly layout that overcame the shortcomings of the original cockpit layout, which was crowded and lacked most of the desired man-machine interface characteristics. It incorporated a head-up display (HUD), eye-level multifunction color displays, hands on throttle and stick control (HOTAS), solid-state charge coupled device (CCD) camera, videotape recorder, and a one-piece windshield.

 

The MiG-21 2000 could be equipped with a display and sight helmet (DASH) system, supplied by Elbit of Haifa, which enabled the pilot to aim the weapons simply by looking at the target. The system worked by measuring the pilot's line of sight relative to the aircraft, and transferred the information to the aircraft's sensors, avionics and weapon systems. The helmet displayed vital information, such as the missile line of sight, missile status, flight information and warning data, on the visor. The DASH helmet allowed the pilot to fly head-up and off-boresight and assisted the pilot to detect, identify and shoot earlier.

 

IAI Lahav's upgrade package could be tailored to meet the customer's specific operational and budgetary requirements - the Lithuanian package included the radar, cockpit and also the DASH update and was rumored to cost around 4 Mio. USD per aircraft, and Lithuania was, together with Romania (where 110 MiG-21 were to be updated), lead customer.

 

As conversion basis, Lithuania purchased fifteen MiG-21 airframes for an unknown sum from the Ukraine, which had inherited a considerable MiG-21 fleet after the demise of the Soviet Union but did not (want to) operate it. The deal included thirteen airworthy MiG-21bis fighters and two MiG-21U trainers with few flying hours on the clocks, and - stripped off any military equipment - the small fleet was gradually transferred as disassembled kits via air ferry in Antonov Airlines An-124 transporters to Aerostar in Romania for conversion, starting in early 1996.

 

The first batch of Lithuanian MiG-21 2000, three fighters and one trainer, arrived in mid-1997 from Bacau on their own power and with civil Ukrainian registrations, and the Lithuanian Air Force’s fighter squadron, the Naikintuvu Eskadra, became ready for service in February 1998.

The rest of the country’s small MiG-21 fleet was delivered in the course of the same year, and these aircraft were semi-officially christened "Globėjas" (Guardian). Since the late Nineties, the Globėjas fighters provide the backbone of Lithuania's air defenses, with aircraft holding Quick Reaction Alert. QRA missions – so-called Alpha Scrambles – have constantly been on the rise thanks to the Russia’s increased aggression towards NATO. The MiG’s have regularly launched to intercept and shadow Russian Air Force Il-20 intelligence gathering aircraft over the Baltic Sea, as well as Tu-16 and Tu-95 patrols and even some Sukhoi Su-27s.

 

Lithuanian pilots use “hit and run” style tactics to deal with air threats, due to the limited range and endurance of their mounts - but this is of little concern due to the country's relatively small size and the defensive nature of the machines' tasks. While the Globėjas lack a beyond-visual range missile, although they could carry one, they have the ability to carry a range of different short-range air-to-air missiles like the Israeli Python III, which Lithuania procured from Rafael in Haifa as primary air-to-air missile.

 

After Lithuania joined NATO organization in 2004, its (alongside Latvia's and Estonia's) air space has been protected by NATO. NATO members provide usually 4 fighter aircraft, based in Lithuania, to police the Baltic States’ airspace, where they support the Lithuanian MiG-21 fleet. The duties rotate between NATO members (which started in March 2004 with Belgium Air Force F-16s) and most NATO members that operate fighters have made temporary deployments to Lithuania.

 

The Lithuanian Globėjas were also in regular demand as a simulated threat, and have gone up against US F-16s, F-15s, F/A-18s and A-10s, as well as the many different European fighter types that frequently rotate into the small country, including the Eurofighter, German F-4F Phantom IIs or French Mirage 2000.

 

Anyway, the Globėjas' airframes sooner or later reached their flying hour limits, and will be phased out towards 2020. As a replacement Lithuania will begin taking delivery of its first batch of ex-Portuguese F-16s in 2016, while the Baltic States are considering in the near future to protect their airspace on their own.

  

General characteristics:

Crew: 1

Length: 14.5 [126] m (47 ft 7 in)

Wingspan: 7.154 m (23 ft 6 in)

Height: 4 m (13 ft 6 in)

Wing area: 23.0 m² (247.3 ft²)

Empty weight: 5,846 kg (12,880 lb)

Gross weight: 8,825 kg (19,425 lb)

 

Powerplant:

1× Tumansky R25-300, rated at 40.21 kN (9,040 lbf) thrust dry

and 69.62 kN (15,650 lbf) with afterburner

 

Performance:

Maximum speed: 2,175 km/h (1,351.48 mph)

Maximum speed: Mach 2.0

Landing speed: 350 km/h (190 kts)

Range: (internal fuel) 1,210 km (751 miles)

Service ceiling: 17,800 m (58,400 ft)

Rate of climb: 225 m/s (44,280 ft/min)

 

Armament:

1x internal 23 mm GSh-23 cannon

5x hardpoints for a wide range of guided and unguided ordnance of up to 3.310 lb (1.500 kg).

 

In QRA configuration the Lithuanian MiG-21 typically carry two or four Rafal Python III short

range air-to-air missiles and an 800l drop tank on the centerline pylon.

Against ground targets, unguided bombs of up to 1.100 lb (500kg) caliber or unguided rockets

can be carried; alternatively, a Rafael LITENING laser designation pod and three

Griffin Mk. 82 LGBs or a single Mk. 84 LGB can be carried, or optically guided weapons like up

to four AGM-65 Maverick or a single GBU-8.

  

The kit and its assembly:

This kit is the entry for the 2016 "One Week Group Build" at whatifmodelers.com, which ran from 29th of April until 8th May (so, actually nine days...). I had this project earmarked for the recent "Cold War" GB, but it fell outside of the build's time horizon. But despite the dubious kit as basis, I tackled the build since I had anything else already at hand.

 

The basis is the MiG-21-93 demonstrator kit from Ukrainian manufacturer Condor, one of the many reincarnations of the venerable KP MiG-21bis, but with some updates. You get, for instance, engraved, very fine panel lines, some typical details were added like the wraparound windscreen (wrong shape, though) and the radar warning fairing on the fin as well as an extra sprue with modern Russian ordnance – apparently from some other kit!

On the downside, there's overall mediocre fit due to the molds' age, some dubious details (anything appears softened or blurred…) or the simple lack thereof (e. g. there’s no ventral gun fairing at all). But there’s nothing that could not be mended, and after all this is just a whiffy version.

 

Since there was only one week time to build the thing and make beauty pics, the whole project remained close to OOB status, even though a lot of detail changes or additions were made in order to convert the Russian MiG-21-93 into an earlier but similar Israeli MiG-21 2000 derivative.

 

These mods include:

- A Martin Baker ejection seat, with wire trigger handles

- HUD made from clear styrene

- Lowered flaps

- An added jet pipe/interior for the otherwise bleak exhaust (parts from a Kangnam Yak-38)

- Hydraulic pipes on the landing gear, made from very thin wire

- Some more/different blade antennae

- Measuring vanes on the pitot boom

- Different GSh-23 gun fairing, from an Academy MiG-23

- Thinner blast deflector plates under the anti-surge doors

- A pair of Python III AAMs, plus respective launch rails

- Different centerline drop tank, from an F-5E

- Scratched chaff/flare dispensers under the rear fuselage (as carried by the MiG-21 2000 demonstrator)

 

Building the model went straightforward, but it took some putty work to fill some seams, dents and holes all around the kit. Biggest issue was a hole in front of the cockpit screen, where simply not enough styrene had been injected into the mould!

  

Painting and markings:

The Lithuanian Air Force as operator for this build was chosen because it would not only fit into the real world timeline (even though I doubt that there would have been any budget for this aircraft at that time, even if MiG-21s had not been upgraded at all...) and because the potential livery would be very simple: contemporary L-39 trainers, C-27L Spartan as well as some L-410 and Mi-8 transporters carry a uniform, dull grey livery. Why not apply it on an air superiority fighter, too?

 

Finding an appropriate tone was not easy, though. Some sources claim the grey tone to be FS 36306, others refer to FS 36270 or "close to Blue/Grey FS35237", but IMHO none of the cited Federal Standard tones works well. Real world Lithuanian aircraft appear pretty dark and dull, and the color also features a greenish, slate grey hue - it's a unique color indeed.

 

After some trials (and also wishing to avoid mixing) I settled for Humbrol 111 (German Field Grey, a.k.a. Uniform Grey) as basic tone. It's a rather dark choice, but I wanted some good contrast to the national markings. A full wraparound livery appeared a little too dark and boring, so I added light blue wing undersurfaces (Humbrol 115). The kit received a light black in wash and some panel shading, primarily in order to add some life to the otherwise uniform surface.

 

Details were painted according to real world MiG-21 pics: the cockpit became classic teal with light grey instrument panels, plus OOB decals for the dashboard and side consoles. The landing gear struts were painted in a light, metallic grey (Humbrol 127 + 56) while the wells were painted in an odd primer color, a mix of Aluminum, Sand and Olive Drab. Parts of the covers were painted with Humbrol 144 (Blue Grey), seen on a modernized real world MiG-21. The wheel discs became bright green.

 

IAI's MiG-21 2000 demonstrator from 1993 had a black radome (as well as later Romanian LanceR Cs), so I adapted this detail for my build. Other typical di-electric fairings on a MiG-21's hull were painted in slightly darker camouflage colors, while the fin's leading edge became dark grey.

The blast deflector plates received yellow and black warning stripes, and some potentially dangerous parts for the ground crews like the pointed anti-flutter booms were painted red. The Python IIIs were simply painted all-white, mounted on grey launch rails - a harsh contrast to the dull rest of the aircraft.

 

Main markings come from a Blue Rider Publishing aftermarket sheet for modern Lithuanian aircraft. This set also includes the small Air Force crests, which I put on the nose, as well as the typical, blue tactical codes.

The stencils come from the scrap box, the small Lithuanian flag stripes on the tail rudder were created from single decal stripes, a personal addition inspired by Lithuanian C-27J transporters. They add some more color to the otherwise murky Baltic MiG fighter.

The silver ring around the air intake as well as the stripes at the flaps and the rudder were created with simple decal stripes instead of paint.

 

Finally, after I added some graphite soot around the jet exhaust and some panle lines with a pencil (e .g. the blow-in doors and airbrake outlines), the kit was sealed with hardly thinned Revell matt acrylic varnish, trying to create a really dull finish.

  

A tough build, despite being mostly OOB, but the details took their toll. This Baltic MiG does not look flashy, but, with IAI's real world MiG-21 2000 as well as the LanceR conversion for Romania in the Nineties, this one is pretty plausible. And with the simple paint scheme, the MiG-21 looks even pretty chic!

BF-4 Flt 508 Mr. Peter Wilson and BF-5 Flt 370 Sqn Ldr Andy Adgell fly from HMS Queen Elizabeth on 27 Sep 2018

  

From Wikipedia, the free encyclopedia

 

The Lockheed Martin F-35 Lightning II is a family of single-seat, single-engine, all-weather, stealth, fifth-generation, multirole combat aircraft, designed for ground-attack and air-superiority missions. It is built by Lockheed Martin and many subcontractors, including Northrop Grumman, Pratt & Whitney, and BAE Systems.

 

The F-35 has three main models: the conventional takeoff and landing F-35A (CTOL), the short take-off and vertical-landing F-35B (STOVL), and the catapult-assisted take-off but arrested recovery, carrier-based F-35C (CATOBAR). The F-35 descends from the Lockheed Martin X-35, the design that was awarded the Joint Strike Fighter (JSF) program over the competing Boeing X-32. The official Lightning II name has proven deeply unpopular and USAF pilots have nicknamed it Panther, instead.

 

The United States principally funds F-35 development, with additional funding from other NATO members and close U.S. allies, including the United Kingdom, Italy, Australia, Canada, Norway, Denmark, the Netherlands, and formerly Turkey. These funders generally receive subcontracts to manufacture components for the aircraft; for example, Turkey was the sole supplier of several F-35 parts until its removal from the program in July 2019. Several other countries have ordered, or are considering ordering, the aircraft.

 

As the largest and most expensive military program ever, the F-35 became the subject of much scrutiny and criticism in the U.S. and in other countries. In 2013 and 2014, critics argued that the plane was "plagued with design flaws", with many blaming the procurement process in which Lockheed was allowed "to design, test, and produce the F-35 all at the same time," instead of identifying and fixing "defects before firing up its production line". By 2014, the program was "$163 billion over budget [and] seven years behind schedule". Critics also contend that the program's high sunk costs and political momentum make it "too big to kill".

 

The F-35 first flew on 15 December 2006. In July 2015, the United States Marines declared its first squadron of F-35B fighters ready for deployment. However, the DOD-based durability testing indicated the service life of early-production F-35B aircraft is well under the expected 8,000 flight hours, and may be as low as 2,100 flight hours. Lot 9 and later aircraft include design changes but service life testing has yet to occur. The U.S. Air Force declared its first squadron of F-35As ready for deployment in August 2016. The U.S. Navy declared its first F-35Cs ready in February 2019. In 2018, the F-35 made its combat debut with the Israeli Air Force.

 

The U.S. stated plan is to buy 2,663 F-35s, which will provide the bulk of the crewed tactical airpower of the U.S. Air Force, Navy, and Marine Corps in coming decades. Deliveries of the F-35 for the U.S. military are scheduled until 2037 with a projected service life up to 2070.

 

Development

 

F-35 development started in 1992 with the origins of the Joint Strike Fighter (JSF) program and was to culminate in full production by 2018. The X-35 first flew on 24 October 2000 and the F-35A on 15 December 2006.

 

The F-35 was developed to replace most US fighter jets with the variants of a single design that would be common to all branches of the military. It was developed in co-operation with a number of foreign partners, and, unlike the F-22 Raptor, intended to be available for export. Three variants were designed: the F-35A (CTOL), the F-35B (STOVL), and the F-35C (CATOBAR). Despite being intended to share most of their parts to reduce costs and improve maintenance logistics, by 2017, the effective commonality was only 20%. The program received considerable criticism for cost overruns during development and for the total projected cost of the program over the lifetime of the jets.

 

By 2017, the program was expected to cost $406.5 billion over its lifetime (i.e. until 2070) for acquisition of the jets, and an additional $1.1 trillion for operations and maintenance. A number of design deficiencies were alleged, such as: carrying a small internal payload; performance inferior to the aircraft being replaced, particularly the F-16; lack of safety in relying on a single engine; and flaws such as the vulnerability of the fuel tank to fire and the propensity for transonic roll-off (wing drop). The possible obsolescence of stealth technology was also criticized.

  

Design

 

Overview

 

Although several experimental designs have been developed since the 1960s, such as the unsuccessful Rockwell XFV-12, the F-35B is to be the first operational supersonic STOVL stealth fighter. The single-engine F-35 resembles the larger twin-engined Lockheed Martin F-22 Raptor, drawing design elements from it. The exhaust duct design was inspired by the General Dynamics Model 200, proposed for a 1972 supersonic VTOL fighter requirement for the Sea Control Ship.

 

Lockheed Martin has suggested that the F-35 could replace the USAF's F-15C/D fighters in the air-superiority role and the F-15E Strike Eagle in the ground-attack role. It has also stated the F-35 is intended to have close- and long-range air-to-air capability second only to that of the F-22 Raptor, and that the F-35 has an advantage over the F-22 in basing flexibility and possesses "advanced sensors and information fusion".

 

Testifying before the House Appropriations Committee on 25 March 2009, acquisition deputy to the assistant secretary of the Air Force, Lt. Gen. Mark D. "Shack" Shackelford, stated that the F-35 is designed to be America's "premier surface-to-air missile killer, and is uniquely equipped for this mission with cutting-edge processing power, synthetic aperture radar integration techniques, and advanced target recognition".

 

Improvements

Ostensible improvements over past-generation fighter aircraft include:

 

Durable, low-maintenance stealth technology, using structural fiber mat instead of the high-maintenance coatings of legacy stealth platforms

Integrated avionics and sensor fusion that combine information from off- and on-board sensors to increase the pilot's situational awareness and improve target identification and weapon delivery, and to relay information quickly to other command and control (C2) nodes

High-speed data networking including IEEE 1394b and Fibre Channel (Fibre Channel is also used on Boeing's Super Hornet.

The Autonomic Logistics Global Sustainment, Autonomic Logistics Information System (ALIS), and Computerized maintenance management system to help ensure the aircraft can remain operational with minimal maintenance manpower The Pentagon has moved to open up the competitive bidding by other companies. This was after Lockheed Martin stated that instead of costing 20% less than the F-16 per flight hour, the F-35 would actually cost 12% more. Though the ALGS is intended to reduce maintenance costs, the company disagrees with including the cost of this system in the aircraft ownership calculations. The USMC has implemented a workaround for a cyber vulnerability in the system. The ALIS system currently requires a shipping-container load of servers to run, but Lockheed is working on a more portable version to support the Marines' expeditionary operations.

Electro-hydrostatic actuators run by a power-by-wire flight-control system

A modern and updated flight simulator, which may be used for a greater fraction of pilot training to reduce the costly flight hours of the actual aircraft

Lightweight, powerful lithium-ion batteries to provide power to run the control surfaces in an emergency

Structural composites in the F-35 are 35% of the airframe weight (up from 25% in the F-22). The majority of these are bismaleimide and composite epoxy materials. The F-35 will be the first mass-produced aircraft to include structural nanocomposites, namely carbon nanotube-reinforced epoxy. Experience of the F-22's problems with corrosion led to the F-35 using a gap filler that causes less galvanic corrosion to the airframe's skin, designed with fewer gaps requiring filler and implementing better drainage. The relatively short 35-foot wingspan of the A and B variants is set by the F-35B's requirement to fit inside the Navy's current amphibious assault ship parking area and elevators; the F-35C's longer wing is considered to be more fuel efficient.

 

Costs

A U.S. Navy study found that the F-35 will cost 30 to 40% more to maintain than current jet fighters, not accounting for inflation over the F-35's operational lifetime. A Pentagon study concluded a $1 trillion maintenance cost for the entire fleet over its lifespan, not accounting for inflation. The F-35 program office found that as of January 2014, costs for the F-35 fleet over a 53-year lifecycle was $857 billion. Costs for the fighter have been dropping and accounted for the 22 percent life cycle drop since 2010. Lockheed stated that by 2019, pricing for the fifth-generation aircraft will be less than fourth-generation fighters. An F-35A in 2019 is expected to cost $85 million per unit complete with engines and full mission systems, inflation adjusted from $75 million in December 2013.

Two Lockheed Martin F-35B Lightning II fighter jets have successfully landed on board HMS Queen Elizabeth for the first time, laying the foundations for the next 50 years of fixed wing aviation in support of the UK’s Carrier Strike Capability.

 

Royal Navy Commander, Nathan Gray, 41, made history by being the first to land on board HMS Queen Elizabeth, carefully maneuvering his stealth jet onto the thermal coated deck. He was followed by Squadron Leader Andy Edgell, RAF, both of whom are test pilots, operating with the Integrated Test Force (ITF) based at Naval Air Station Patuxent River, Maryland.

 

Shortly afterwards, once a deck inspection has been conducted and the all-clear given, Cmdr Gray became the first pilot to take off using the ship’s ski-ramp.

  

From Wikipedia, the free encyclopedia

 

The Lockheed Martin F-35 Lightning II is a family of single-seat, single-engine, all-weather, stealth, fifth-generation, multirole combat aircraft, designed for ground-attack and air-superiority missions. It is built by Lockheed Martin and many subcontractors, including Northrop Grumman, Pratt & Whitney, and BAE Systems.

 

The F-35 has three main models: the conventional takeoff and landing F-35A (CTOL), the short take-off and vertical-landing F-35B (STOVL), and the catapult-assisted take-off but arrested recovery, carrier-based F-35C (CATOBAR). The F-35 descends from the Lockheed Martin X-35, the design that was awarded the Joint Strike Fighter (JSF) program over the competing Boeing X-32. The official Lightning II name has proven deeply unpopular and USAF pilots have nicknamed it Panther, instead.

 

The United States principally funds F-35 development, with additional funding from other NATO members and close U.S. allies, including the United Kingdom, Italy, Australia, Canada, Norway, Denmark, the Netherlands, and formerly Turkey. These funders generally receive subcontracts to manufacture components for the aircraft; for example, Turkey was the sole supplier of several F-35 parts until its removal from the program in July 2019. Several other countries have ordered, or are considering ordering, the aircraft.

 

As the largest and most expensive military program ever, the F-35 became the subject of much scrutiny and criticism in the U.S. and in other countries. In 2013 and 2014, critics argued that the plane was "plagued with design flaws", with many blaming the procurement process in which Lockheed was allowed "to design, test, and produce the F-35 all at the same time," instead of identifying and fixing "defects before firing up its production line". By 2014, the program was "$163 billion over budget [and] seven years behind schedule". Critics also contend that the program's high sunk costs and political momentum make it "too big to kill".

 

The F-35 first flew on 15 December 2006. In July 2015, the United States Marines declared its first squadron of F-35B fighters ready for deployment. However, the DOD-based durability testing indicated the service life of early-production F-35B aircraft is well under the expected 8,000 flight hours, and may be as low as 2,100 flight hours. Lot 9 and later aircraft include design changes but service life testing has yet to occur. The U.S. Air Force declared its first squadron of F-35As ready for deployment in August 2016. The U.S. Navy declared its first F-35Cs ready in February 2019. In 2018, the F-35 made its combat debut with the Israeli Air Force.

 

The U.S. stated plan is to buy 2,663 F-35s, which will provide the bulk of the crewed tactical airpower of the U.S. Air Force, Navy, and Marine Corps in coming decades. Deliveries of the F-35 for the U.S. military are scheduled until 2037 with a projected service life up to 2070.

 

Development

 

F-35 development started in 1992 with the origins of the Joint Strike Fighter (JSF) program and was to culminate in full production by 2018. The X-35 first flew on 24 October 2000 and the F-35A on 15 December 2006.

 

The F-35 was developed to replace most US fighter jets with the variants of a single design that would be common to all branches of the military. It was developed in co-operation with a number of foreign partners, and, unlike the F-22 Raptor, intended to be available for export. Three variants were designed: the F-35A (CTOL), the F-35B (STOVL), and the F-35C (CATOBAR). Despite being intended to share most of their parts to reduce costs and improve maintenance logistics, by 2017, the effective commonality was only 20%. The program received considerable criticism for cost overruns during development and for the total projected cost of the program over the lifetime of the jets.

 

By 2017, the program was expected to cost $406.5 billion over its lifetime (i.e. until 2070) for acquisition of the jets, and an additional $1.1 trillion for operations and maintenance. A number of design deficiencies were alleged, such as: carrying a small internal payload; performance inferior to the aircraft being replaced, particularly the F-16; lack of safety in relying on a single engine; and flaws such as the vulnerability of the fuel tank to fire and the propensity for transonic roll-off (wing drop). The possible obsolescence of stealth technology was also criticized.

  

Design

 

Overview

 

Although several experimental designs have been developed since the 1960s, such as the unsuccessful Rockwell XFV-12, the F-35B is to be the first operational supersonic STOVL stealth fighter. The single-engine F-35 resembles the larger twin-engined Lockheed Martin F-22 Raptor, drawing design elements from it. The exhaust duct design was inspired by the General Dynamics Model 200, proposed for a 1972 supersonic VTOL fighter requirement for the Sea Control Ship.

 

Lockheed Martin has suggested that the F-35 could replace the USAF's F-15C/D fighters in the air-superiority role and the F-15E Strike Eagle in the ground-attack role. It has also stated the F-35 is intended to have close- and long-range air-to-air capability second only to that of the F-22 Raptor, and that the F-35 has an advantage over the F-22 in basing flexibility and possesses "advanced sensors and information fusion".

 

Testifying before the House Appropriations Committee on 25 March 2009, acquisition deputy to the assistant secretary of the Air Force, Lt. Gen. Mark D. "Shack" Shackelford, stated that the F-35 is designed to be America's "premier surface-to-air missile killer, and is uniquely equipped for this mission with cutting-edge processing power, synthetic aperture radar integration techniques, and advanced target recognition".

 

Improvements

Ostensible improvements over past-generation fighter aircraft include:

 

Durable, low-maintenance stealth technology, using structural fiber mat instead of the high-maintenance coatings of legacy stealth platforms

Integrated avionics and sensor fusion that combine information from off- and on-board sensors to increase the pilot's situational awareness and improve target identification and weapon delivery, and to relay information quickly to other command and control (C2) nodes

High-speed data networking including IEEE 1394b and Fibre Channel (Fibre Channel is also used on Boeing's Super Hornet.

The Autonomic Logistics Global Sustainment, Autonomic Logistics Information System (ALIS), and Computerized maintenance management system to help ensure the aircraft can remain operational with minimal maintenance manpower The Pentagon has moved to open up the competitive bidding by other companies. This was after Lockheed Martin stated that instead of costing 20% less than the F-16 per flight hour, the F-35 would actually cost 12% more. Though the ALGS is intended to reduce maintenance costs, the company disagrees with including the cost of this system in the aircraft ownership calculations. The USMC has implemented a workaround for a cyber vulnerability in the system. The ALIS system currently requires a shipping-container load of servers to run, but Lockheed is working on a more portable version to support the Marines' expeditionary operations.

Electro-hydrostatic actuators run by a power-by-wire flight-control system

A modern and updated flight simulator, which may be used for a greater fraction of pilot training to reduce the costly flight hours of the actual aircraft

Lightweight, powerful lithium-ion batteries to provide power to run the control surfaces in an emergency

Structural composites in the F-35 are 35% of the airframe weight (up from 25% in the F-22). The majority of these are bismaleimide and composite epoxy materials. The F-35 will be the first mass-produced aircraft to include structural nanocomposites, namely carbon nanotube-reinforced epoxy. Experience of the F-22's problems with corrosion led to the F-35 using a gap filler that causes less galvanic corrosion to the airframe's skin, designed with fewer gaps requiring filler and implementing better drainage. The relatively short 35-foot wingspan of the A and B variants is set by the F-35B's requirement to fit inside the Navy's current amphibious assault ship parking area and elevators; the F-35C's longer wing is considered to be more fuel efficient.

 

Costs

A U.S. Navy study found that the F-35 will cost 30 to 40% more to maintain than current jet fighters, not accounting for inflation over the F-35's operational lifetime. A Pentagon study concluded a $1 trillion maintenance cost for the entire fleet over its lifespan, not accounting for inflation. The F-35 program office found that as of January 2014, costs for the F-35 fleet over a 53-year lifecycle was $857 billion. Costs for the fighter have been dropping and accounted for the 22 percent life cycle drop since 2010. Lockheed stated that by 2019, pricing for the fifth-generation aircraft will be less than fourth-generation fighters. An F-35A in 2019 is expected to cost $85 million per unit complete with engines and full mission systems, inflation adjusted from $75 million in December 2013.

 

Landmark Accomplishments:

Longest highway tunnel in North America (13,300' or 2.5 miles).

Longest combined rail and highway use tunnel in North America.

First U.S. tunnel with jet turbine and portal fan ventilation.

First computerized regulation of both rail and highway traffic.

First tunnel designed for -40° F. and 150 mph winds.

Portal buildings designed to withstand avalanches

The position of titular organist ("head" or "chief" organist) at Notre-Dame is considered one of the most prestigious organist posts in France, along with the post of titular organist of Saint Sulpice in Paris, Cavaillé-Coll's largest instrument.

 

The organ has 7,374 pipes, with ca 900 classified as historical. It has 110 real stops, five 56-key manuals and a 32-key pedalboard. In December 1992, a two-year restoration of the organ was completed that fully computerized the organ under three LANs (Local Area Networks).

A seamstress is a woman who sews for a living.

Sewing is the craft of fastening or attaching objects using stitches made with a needle and thread. Sewing is one of the oldest of the textile arts, arising in the Paleolithic era. Before the discovery of spinning yarn or weaving fabric, archaeologists believe Stone Age people across Europe and Asia sewed fur and skin clothing using bone, antler or ivory needles and "thread" made of various animal body parts including sinew, catgut, and veins. Although usually associated with clothing and household linens, sewing is used in a variety of crafts and industries, including shoemaking, upholstery, sailmaking, bookbinding and the manufacturing of some kinds of sporting goods. Sewing is the fundamental process underlying a variety of textile arts and crafts, including embroidery, tapestry, quilting, appliqué and patchwork.

For thousands of years, all sewing was done by hand. The invention of the sewing machine in the 19th century and the rise of computerization in the later 20th century led to mass production of sewn objects, but hand sewing is still practiced around the world. Fine hand sewing is a characteristic of high-quality tailoring, haute couture fashion, and custom dressmaking, and is pursued by both textile artists and hobbyists as a means of creative expression.-Wikipedia

Contains historic images of the 1969 moonwalk.

 

Before computerized simulation, there was Viewmaster, which--along with imagination--educated my generation. Found at "Curiosities," a fabulous treasure trove of antiques, folk art and supplies for the assemblage artist in Dallas, TX.

taken for Our Daily Challenge - stopped action

 

I wanted to do a wave today but there wasn't enough wind to produce anything more than a gentle swell today so I tried for a fast enough speed to stop the water action of the fountains instead. The photo above and below depicts one of the Maids of the Mist, an icon of St. Joseph. Constance faces West and behind her, facing East is Hope.

 

The one that looks like a nozzle below is in the compass fountain in St. Joseph. Most of the time jets go straight up from the ground in the area of the compass but at selected times during the hour the ground jets stop and instead the nozzles (cannons) surrounding the compass all begin to spray into its center. It was actually too busy today to get good shots because it was so crowded. The best time is when there are just a dozen or so kids playing in it. I'll link a few I took last year so you can get a better idea of it.

 

Facts about the compass fountain:

1. Concrete inner splash pad is 150 ft. in diameter

2. Outer ring of the pad is 200 ft. in diameter

3. There are 28 varying height water jets

4. These water jets supply 785 gallons of water per minute

5. There are 5 computerized light shows available

6. There are 8 water cannons mounted on armillary spheres

7. Cannons are equipped with 1000 watt lights

8. These cannons spray water 35 ft. into the air

9. The cannons supply 2,560 gallons of water per minute

10. The water reservoir holds 10,860 gallons of recycled water

 

Saudi Arabia was interested in acquiring the F-15E for its air force, but the aircraft was deemed too sensitive for export. As an alternative, Saudi Arabia requested the delivery of 24 F-15Fs, which were similar to the F-15E but without the second crew member and without some of the more advanced avionics deemed too sensitive for export. However, in 1993, the Royal Saudi Air Force was given permission to purchase 72 slightly downgraded versions of the F-15E Strike Eagle, initially designated F-15XP but now known as F-15S. The F-15S has an APG-70S radar that is "detuned" from the capabilities of the APG-63 of the F-15C/D and does not have the ability to do computerized ground mapping. It has only 60 percent of the bandwidth of the APG-63 and is limited to only 16 rather than 32 channels. The AWG-27 programmable armament control set was reprogrammed to prevent the carriage of certain weapons systems, and the hands-off automatic terrain following mode was deleted from the ASW-51 autopilot. A ring laser gyro INS was provided, but the military-grade GPS system was eliminated, although the Saudis have added a commercial-grade GPS system.

 

Some sensitive ECM systems are replaced with older equipment or are deleted altogether. The nuclear weapon wiring fitted to USAF F-15Es was deleted. Some initial reports indicated that the F-15S would not be provided with the ability to carry conformal fuel tanks and their associated weapons pylons, but this turned out not to be the case. Saudi Arabia received 48 downgraded versions of the Martin Marietta LANTIRN system known as AAQ-19 Sharpshooter, as well as the AAQ-20 Pathfinder, which is a simplified version of the AAQ-13 Nav-Pod. The AAQ-20 is not compatible with the AGM-65 Maverick air-to-ground missile and has some air-to-air features deleted.

 

In this image, an F-15S (F-15S-59-MC, serial number 93-0913 reserialed to 9225) from the 6 Squadron, Wing 5 stationed at King Khalid AB near Khamis Mushait flies over the western Arabian desert. A total of 72 were placed on order under Peace Sun IX. The first example took off on its maiden flight on 19 June 1995. Production was planned at a rate of one per month, with the 72nd and last F-15S being delivered in 1999. A new variant, the F-15SA (Saudi Advanced), is under development and will have a new fly-by-wire flight control system and the APG-63(v)3 active electronically scanned array (AESA) radar, digital electronic warfare systems (DEWS), and infrared search and track (IRST) systems. It will also have a redesigned cockpit, once intended for the F-15SE Silent Eagle.

+++ DISCLAIMER +++

Nothing you see here is real, even though the conversion or the presented background story might be based historical facts. BEWARE!

 

Some background:

The Northrop Grumman-IAI F-24 is the latest reincarnation of the USAF "Lightweight Fighter Program" which dates back to the 1950ies and started with the development of Northrop's F-5 "Freedom Fighter".

 

The 1st generation F-5 became very successful in the export market and saw a long line of development, including the much more powerful F-5E "Tiger II" and the F-20 Tigershark (initially called F-5G). Northrop had high hopes for the F-20 in the international market; however, policy changes following Ronald Reagan's election meant the F-20 had to compete for sales against aircraft like the F-16, the USAF's latest fighter design (which was politically favored). The F-20 development program was eventually abandoned in 1986 after three prototypes had been built and a fourth partially completed.

 

But this was not the end for Northrop’s Lightweight Fighter. In the early 1980s, two X-29As experimental aircraft were built by Grumman from two existing Northrop F-5A Freedom Fighter airframes. The Grumman X-29 was a testbed for forward-swept wings, canard control surfaces, and other novel aircraft technologies. The aerodynamic instability of this arrangement increased agility but required the use of computerized fly-by-wire control. Composite materials were used to control the aeroelastic divergent twisting experienced by forward-swept wings, also reducing the weight. The NASA test program continued from 1984 to 1991 and the X-29s flew 242 times, gathering valuable data and breaking ground for new aerodynamic technologies of 4th and 5th generation fighters.

 

Even though no service aircraft directly evolved from the X-29, its innovative FBW system as well as the new material technologies also opened the door for an updated F-20 far beyond the 1990ies. It became clear that ever expensive and complex aircraft could not be the answer to modern, asymmetrical warfare in remote corners of the world, with exploding development costs and just a limited number of aircraft in service that could not generate true economies of scale, esp. when their state-of-the-art design would not permit any export.

Anyway, a global market for simpler fighter aircraft was there, as 1st generation F-16s as well as the worldwide, aging F-5E fleet and types of Soviet/Russian origin like the MiG-29 provided the need for a modern, yet light and economical jet fighter. Contemporary types like the Indian HAL Tejas, the Swedish Saab Gripen, the French Dassault Rafale and the Pakistani/Chinese FC-1/JF-17 ”Thunder” proved this trend among 4th - 4.5th generation fighter aircraft.

 

Northrop Grumman (Northrop bought Grumman in 1994) initiated studies and basic design work on a respective New Lightweight Fighter (NLF) as a private venture in 1995. Work on the NLF started at a slow pace, as the company was busy with re-structuring.

The idea of an updated lightweight fighter was fueled by another source, too: Israel. In 1998 IAI started looking in the USA for a development partner for a new, light fighter that would replace its obsolete Kfir fleet and partly relieve its F-16 and F-15 fleet from interception tasks. The domestic project for that role, the IAI Lavi, had been stillborn, but lots of its avionics and research were still at hand and waited for an airframe for completion.

The new aircraft for the IAF was to be superior to the MiG-29, at least on par with the F-16C/D, but easier to maintain, smaller and overall cheaper. Since the performance profiles appeared to be similar to what Northrop Grumman was developing under the NLF label, the US company eventually teamed up with IAI in 2000 and both started the mutual project "Namer" (=נמר, “Tiger” in Hebrew), which eventually lead to the F-24 I for the IAF which kept its project name for service and to the USAF’s F-24A “Tigershark”.

 

The F-24, as the NLF, was based on the F-20 airframe, but outwardly showed only little family heritage, onle the forward fuselage around the cockpit reminds of the original F-5 design . Many aerodynamic details, e. g. the air intakes and air ducts, were taken over from the X-29, though, as the experimental aircraft and its components had been developed for extreme maneuvers and extra high agility. Nevertheless, the X-29's forward-swept wing was considered to be too exotic and fragile for a true service aircraft, but the F-24 was to feature an Active Aeroelastic Wing (AAW) system.

 

AAW Technology integrates wing aerodynamics, controls, and structure to harness and control wing aeroelastic twist at high speeds and dynamic pressures. By using multiple leading and trailing edge controls like "aerodynamic tabs", subtle amounts of aeroelastic twist can be controlled to provide large amounts of wing control power, while minimizing maneuver air loads at high wing strain conditions or aerodynamic drag at low wing strain conditions. This system was initially tested on the X-29 and later on the X-53 research aircraft, a modified F-18, until 2006.

 

Both USAF and IAF versions feature this state-of-the-art aerodynamic technology, but it is uncertain if other customers will receive it. While details concerning the F-24's system have not been published yet, it is assumed that its AAW is so effective that canard foreplanes could be omitted without sacrificing lift and maneuverability, and that drag is effectively minimized as the wing profile can be adjusted according to the aircraft’s speed, altitude, payload and mission – much like a VG wing, but without its clumsy and heavy swiveling mechanism which has to bear high g forces. As a result, the F-24 is, compared to the F-20, which could carry an external payload of about 3.5 tons, rumored to be able to carry up to 5 tons of ordnance.

 

The delta wing shape proved to be a perfect choice for the required surface and flap actuators inside of the wings, and it would also offer a very good compromise between lift and drag for a wide range of performance. Anyway, there was one price to pay: in order to keep the wing profile thin and simple, the F-24’s landing gear retracts into the lower fuselage, leaving the aircraft with a relatively narrow track.

 

Another major design factor for the outstanding performance of this rather small aircraft was weight reduction and structural integrity – combined with simplicity, ruggedness and a modular construction which would allow later upgrades. Instead of “going big” and expensive, the new F-24 was to create its performance through dedicated loss of weight, which was in some part also a compensation for the AAW system in the wings and its periphery.

 

Weight was saved wherever possible, e .g. a newly developed, lightweight M199A1 gatling gun. This 20mm cannon is a three-barreled, heavily modified version of the already “stripped” M61A2 gun in the USAF’s current F-18E and F-22. One of the novel features is a pneumatic drive instead of the traditional electric mechanism, what not only saves weight but also improves trigger response. The new gun weighs only a mere 65kg (the six-barreled M61A2 weighs 92kg, the original M61A1 112 kg), but still reaches a burst rate of fire of 1.800 RPM (about 800 RPM under cyclic fire, standard practice is to fire the cannon in 30 to 50-round bursts, though) and a muzzle velocity of 1.050 metres per second (3,450 ft/s) with a PGU-28/B round.

 

While the F-16 was and is still made from 80% aluminum alloys and only from 3% composites, the F-24 makes major use of carbon fiber and other lightweight materials, which make up about 40% of the aircraft’s structure, plus an increased share of Titanium and Magnesium alloys. As a consequence and through many other weight-saving measures like keeping stealth capabilities to a minimum (even though RAM was deliberately used and many details designed to have a natural low radar signature, resulting in modest radar cross-section (RCS) reductions), a single, relatively small engine, a fuel-efficient F404-GE-402 turbofan, is enough to make the F-24 a fast and very agile aircraft, coupled with a good range. The F-24’s thrust/weight ratio is considerably higher than 1, and later versions with a vectored thrust nozzle (see below) will take this level of agility even further – with the pilot becoming the limiting factor for the aircraft’s performance.

 

USAF and IAF F-24s are outfitted with Northrop Grumman's AN/APG-80 Active Electronically Scanned Array (AESA) radar, also used in the F-16 Block 60 aircraft. Other customers might only receive the AN/APG-68, making the F-24 comparable to the F-16C/D.

 

The first prototype, the YF-24, flew on 8th of March 2008, followed by two more aircraft plus a static airframe until summer 2010. In early 2011 the USAF placed an initial order of 101 aircraft (probably also to stir export sales – the earlier lightweight fighters from Northrop suffered from the fact that the manufacturer’s country would not use the aircraft in its own forces). These initial aircraft will replace older F-16 in the interceptor role, or free them for fighter bomber tasks. The USN and USMC also showed interest in the aircraft for their aggressor squadrons, for dissimilar air combat training. A two-seater, called the F-24B, is supposed to follow soon, too, and a later version for 2020 onwards, tentatively designated F-24C, is to feature an even stronger F404 engine and a 3D vectoring nozzle.

 

Israel is going to produce its own version domestically from late 2014 on, which will exclusively be used by the IAF. These aircraft will be outfitted with different avionics, built by Elta in Israel, and cater to national requirements which focus more on multi-purpose service, while the USAF focusses with its F-24A on aerial combat and interception tasks.

 

International interest for the F-24A is already there: in late 2013 Grumman stated that initial talks have been made with various countries, and potential export candidates from 2015 on are Taiwan, Singapore, Thailand, Finland, Norway, Australia and Japan.

  

General F-24A characteristics:

Crew: 1 pilot

Length: 47 ft 4 in (14.4 m)

Wingspan: 27 ft 11.9 in / 8.53 m; with wingtip missiles (26 ft 8 in/ 8.13 m; without wingtip missiles)

Height: 13 ft 10 in (4.20 m)

Wing area: 36.55 m² (392 ft²)

Empty weight: 13.150 lb (5.090 kg)

Loaded weight: 15.480 lb (6.830 kg)

Max. take-off weight: 27.530 lb (12.500 kg)

 

Powerplant

1× General Electric F404-GE-402 turbofan with a dry thrust of 11,000 lbf (48.9 kN) and 17,750 lbf (79.2 kN) with afterburner

 

Performance

Maximum speed: Mach 2+

Combat radius: 300 nmi (345 mi, 556 km); for hi-lo-hi mission with 2 × 330 US gal (1,250 L) drop tanks

Ferry range: 1,490 nmi (1715 mi, 2759 km); with 3 × 330 US gal (1,250 L) drop tanks

Service ceiling: 55,000 ft (16,800 m)

Rate of climb: 52,800 ft/min (255 m/s)

Wing loading: 70.0 lb/ft² (342 kg/m²)

Thrust/weight: 1.09 (1.35 with loaded weight & 50% fuel)

 

Armament

1× 20 mm (0.787 in) M199A1 3-barreled Gatling cannon in the lower fuselage with 400 RPG

Eleven external hardpoints (two wingtip tails, six underwing hardpoints, three underfuselage hardpoints) and a total capacity of 11.000 lb (4.994 kg) of missiles (incl. AIM 9 Sidewinder and AIM 120 AMRAAM), bombs, rockets, ECM pods and drop tanks for extended range.

  

The kit and its assembly:

A spontaneous project. This major kitbash was inspired by fellow user nighthunter at whatifmodelers.com, who came up with a profile of a mashed-up US fighter, created “out of boredom”. The original idea was called F-21C, and it was to be a domestic successor to the IAI Kfirs which had been used by the US as aggressor aircraft in USN and USMC service for a few years.

 

As a weird(?) coincidence I had many of the necessary ingredients for this fictional aircraft in store, even though some parts and details were later changed. This model here is an interpretation of the original design. The idea was spun further, and the available parts that finally went into the model also had some influence on design and background.

I thank nighthunter for sharing the early ideas, inviting me to take the design to the hardware stage (sort of…) and adapting my feedback into new design sketches, too, which, in return, inspired the model building process.

 

Well, what went into this thing? To cook up a F-24 à la Dizzyfugu you just need (all in 1:72):

● Fuselage from a Hasegawa X-29, including the cockpit and the landing gear

● Fin and nose cone from an Italeri F-16A

● Inner wings from a (vintage) Hasegawa MiG-21F

● Outer wings from a F-4 (probably a J, Hasegawa or Fujimi)

 

The wing construction deviates from nighthunter’s original idea. The favorite ingredients would have been F-16XL or simple Mirage III wings, but I found the composite wing to be more attractive and “different”. The big F-16XL wings, despite their benefit of a unique shape, might also have created scale/size problems with a F-20 style fuselage? So I built hybrid wings: The MiG-21 landing gear wells were filled with putty and the F-4 outer wings simply glued onto the MiG inner wing sections, which were simply cut down in span. It sounds like an unlikely combo, but these parts fit together almost perfectly! In order to hide the F-4 origins I modified them to carry wingtip launch rails, though, which were also part of nighthunter’s original design.

 

The AAW technology detail mentioned in the background came in handy as it explains the complicated wing shape and the fact that the landing gear retracts into the fuselage, not into the wings, which would have been more plausible… Anyway, there’s still room for a simpler export version, with Mirage III or Kfir C.2/7 wings, and maybe canards?

 

Using the X-29 as basis also made fitting the new wings onto the area-ruled fuselage pretty easy, as I could use the wing root parts from the X-29 to bridge the gap. The original, forward-swept wings were just cut away, and the remains used as consoles for the new hybrid delta wings. Took some SERIOUS putty work, but the result is IMHO fine.

 

The bigger/square X-29 air intakes were taken over, and they change the look of the aircraft, making it look less F-5-ish than a true F-20 fuselage. For the same reason I kept the large fairing at the fin base, combining it with a bigger F-16 tail, though, as a counter-balance to the new, bigger wings. Again, the F-16 fin was/is part of nighthunter’s idea, so the model stays true to the original concept.

 

For the same reason I omitted the original X-29 nose, which is rather pointy, sports vanes and a large sensor boom. The F-16 nose was a plausible choice, as the AN/APG-80 is also carried by late Fighting Falcons, and its shape fits well, too.

 

All around the hull, some small details like radar warning sensors, pitots and air scoops were added. Not really necessary, but such thing add IMHO to the overall impression of such a fictional aircraft beyond the prototype stage.

 

Cockpit and landing gear were taken OOB, I just added a pilot figure and slightly modified the seat.

 

The ordnance was puzzled together from the scrap box, the AIM-9Ls come from the same F-4 kit which donated its outer wings, the AIM-120s come from an Italeri NATO weapons kit. The drop tanks belong to an F-16.

  

Painting and markings:

At first I considered an F-24I in IAF markings, or even a Japanese aircraft, but then reverted to one of nighthunter’s initial, simple ideas: an USAF aircraft in the “Hill II” paint scheme (F-16 style), made up from three shades of gray (FS 36118, 36270 and 36375) with low-viz markings and stencils. Dutch/Turkish NF-5A/Bs in the “Hill II” scheme were used as design benchmarks, too. It’s a simple livery, but on this delta wing aircraft it looks pretty interesting. I used enamels, what I had at hand: Humbrol 127 and 126, and Modelmaster's 1723.

 

A light black ink wash was applied, in order to em,phasize the engraved panel lines, in contrast to that, panels were manually highlighted through dry-brushed, lighter shades of gray (Humbrol 27, 166 and 167).

 

“Hill II” also adds to a generic, realistic touch for this whif. Doing an exotic air force thing is rather easy, but creating a convincing whif for a huge military machinery like the USAF’s takes more subtlety, I think.

 

The cockpit was painted in medium Gray (Dark Gull Grey, FS 36231, Humbrol 140), as well as the radome. The landing gear and the air intakes were painted white. The radome was painted with Revell 47 and dry-brushed with Humbrol 140.

 

Decals were puzzled together from various USAF aircraft, including sheets from an Airfix F-117, an Italeri F-15E and even an Academy OV-10D.

  

Tadah: a hardware tribute to an idea, born from boredom - and the aircraft does not look even bad at all? What I wanted to achieve was to make the F-24 neither look like a F-20, nor a Saab Gripen clone, as the latter comes close in overall shape, size and design.

The sign is on the north side of the building. Another ghost sign adorns the south facade.

 

The building at 623 S. Wabash Ave. was constructed in 1895 and designed by Solon S. Beman or the Studebaker Brothers Carriage Company of Fort Wayne, Indiana as its Chicago regional office and warehouse facility. It was later owned by the Brunswick Company, makers of wood furnishings and built-in furniture for libraries, universities and a variety of public commercial and governmental facilities. The building was acquired by Columbia College in 1983 and now houses classrooms, academic offices, a computerized newsroom, sciences laboratories, art studios, stage and costume design workshops and two public gallery spaces.

醫學跳躍性的進步

EMI CT brain scanner, installed at Atkinson Morley's Hospital, Wimbledon in 1971 (the first used clinically), by EMI, Hayes, Middlesex, 1970-1971.

1978年榮總長庚先後引進腦部電腦斷層,從診斷到治療,利用電腦運算回推影像形成或是算出三度空間每一小立方體所得放射劑量,

這都是在我學校時期聞所未聞,而在當住院醫師時趕上第一代腦斷層攝影。

做出這張來紀念。 (Sereotactic body radiotherapy, SBRT)

The Olympus PEN-FT is the most advanced member of the PEN half-format family that flourished in the 1960s. The Pen-F is, all appearances to the contrary, an SLR, but its designers avoided the characteristic hump and bulk of other SLRs by using a Porro prism and fixing it sideways. This required some creative engineering of the shutter design, but the camera's designer, the ingenious Y. Maitani, came up with a brilliant solution there.

 

All film Pens use 35 mm film but the image only takes up half a frame and is exposed sideways, so if you hold the camera horizontally, the picture will be taken in the portrait mode.

 

Olympus offered a large line-up of high quality lenses, but in my opinion, the standard 38/f.1.8 Zuiko lens is also far and away the best choice. Almost always, I find that the field of view is exactly what I need. The lens is fast enough too. Come on. Who needs more aperture than f/1.8?

 

The FT offers off-the-prism (and thus, implicitly, through-the-lens) metering, which makes the viewfinder image a bit darker. Focusing still is a breeze, however, thanks to the microprism focusing screen. The light meter is not coupled - it indicates which f-stop to use, albeit using a proprietary numbering scheme.

 

The web abounds with detailed descriptions of the panoply of technology used in this camera, so I won't talk about that,

 

On a personal note - I find this camera a pure joy to use. There are no frills. It does what it's supposed to do, no more. So I'm not distracted and can concentrate on composing your picture, which is what I should be doing instead of fiddling with controls and menus.

 

You feel, hear and see that it's a brilliant piece of technology. A lot of complex engineering went into making it as simple as it is. Unlike modern computerized DSLRs which appear to be following the tenet that "if it was difficult to engineer it should also be difficult to use."

 

People react to it. Not like they'd react to a high-end DSLR or medium format behemoth. This camera doesn't elicit envy, it just pleases people with its looks. The reaction of the technician in the camera shop today was typical: A small gasp, followed by "Wow, that's a stunner. Let me hear the sound of her." That's right. He said "her", not "it". And then I fired her and his eyes lit up with joy and he went "Ahhhhhh ....yes!"

See what I mean? Everyone who sees her walks off with a smile on their face.

 

This is not a silent camera. But her sound is pure music to anyone who loves cameras. Granted, she has drawbacks.

 

Though she's rather heavy (which is good), the manufacturing quality isn't comparable to, say. a Leica. You see that when she twists and flexes slightly in your hands and you feel it most of all when you advance the film. That has a grindy feel to it.

 

But still. This baby was made in 1966, and I'd say she's in a very admirable state, given that she'll turn 50 next year.

Three Lockheed Martin F-35A-2B "Lightning II" "Joint Strike Fighter's", from the 63rd Fighter Squadron, and a General Dynamics (its aviation unit now part of Lockheed Martin) General Dynamics F-16 "Fighting Falcon", from the 309th Fighter Squadron, fly in formation alongside a Boeing KC-135 "Stratotanker", from the 161st Air Refueling Wing, during a refueling mission near Phoenix Aug. 27, 2019. Six F-35s from the 63rd FS competed in Exercise Panther Beast where the pilots tested their munition dropping accuracy.

  

From Wikipedia, the free encyclopedia

 

The Lockheed Martin F-35 Lightning II is a family of single-seat, single-engine, all-weather, stealth, fifth-generation, multirole combat aircraft, designed for ground-attack and air-superiority missions. It is built by Lockheed Martin and many subcontractors, including Northrop Grumman, Pratt & Whitney, and BAE Systems.

 

The F-35 has three main models: the conventional takeoff and landing F-35A (CTOL), the short take-off and vertical-landing F-35B (STOVL), and the catapult-assisted take-off but arrested recovery, carrier-based F-35C (CATOBAR). The F-35 descends from the Lockheed Martin X-35, the design that was awarded the Joint Strike Fighter (JSF) program over the competing Boeing X-32. The official Lightning II name has proven deeply unpopular and USAF pilots have nicknamed it Panther, instead.

 

The United States principally funds F-35 development, with additional funding from other NATO members and close U.S. allies, including the United Kingdom, Italy, Australia, Canada, Norway, Denmark, the Netherlands, and formerly Turkey. These funders generally receive subcontracts to manufacture components for the aircraft; for example, Turkey was the sole supplier of several F-35 parts until its removal from the program in July 2019. Several other countries have ordered, or are considering ordering, the aircraft.

 

As the largest and most expensive military program ever, the F-35 became the subject of much scrutiny and criticism in the U.S. and in other countries. In 2013 and 2014, critics argued that the plane was "plagued with design flaws", with many blaming the procurement process in which Lockheed was allowed "to design, test, and produce the F-35 all at the same time," instead of identifying and fixing "defects before firing up its production line". By 2014, the program was "$163 billion over budget [and] seven years behind schedule". Critics also contend that the program's high sunk costs and political momentum make it "too big to kill".

 

The F-35 first flew on 15 December 2006. In July 2015, the United States Marines declared its first squadron of F-35B fighters ready for deployment. However, the DOD-based durability testing indicated the service life of early-production F-35B aircraft is well under the expected 8,000 flight hours, and may be as low as 2,100 flight hours. Lot 9 and later aircraft include design changes but service life testing has yet to occur. The U.S. Air Force declared its first squadron of F-35As ready for deployment in August 2016. The U.S. Navy declared its first F-35Cs ready in February 2019. In 2018, the F-35 made its combat debut with the Israeli Air Force.

 

The U.S. stated plan is to buy 2,663 F-35s, which will provide the bulk of the crewed tactical airpower of the U.S. Air Force, Navy, and Marine Corps in coming decades. Deliveries of the F-35 for the U.S. military are scheduled until 2037 with a projected service life up to 2070.

 

Development

 

F-35 development started in 1992 with the origins of the "Joint Strike Fighter" (JSF) program and was to culminate in full production by 2018. The X-35 first flew on 24 October 2000 and the F-35A on 15 December 2006.

 

The F-35 was developed to replace most US fighter jets with the variants of a single design that would be common to all branches of the military. It was developed in co-operation with a number of foreign partners, and, unlike the F-22 Raptor, intended to be available for export. Three variants were designed: the F-35A (CTOL), the F-35B (STOVL), and the F-35C (CATOBAR). Despite being intended to share most of their parts to reduce costs and improve maintenance logistics, by 2017, the effective commonality was only 20%. The program received considerable criticism for cost overruns during development and for the total projected cost of the program over the lifetime of the jets.

 

By 2017, the program was expected to cost $406.5 billion over its lifetime (i.e. until 2070) for acquisition of the jets, and an additional $1.1 trillion for operations and maintenance. A number of design deficiencies were alleged, such as: carrying a small internal payload; performance inferior to the aircraft being replaced, particularly the F-16; lack of safety in relying on a single engine; and flaws such as the vulnerability of the fuel tank to fire and the propensity for transonic roll-off (wing drop). The possible obsolescence of stealth technology was also criticized.

  

Design

 

Overview

 

Although several experimental designs have been developed since the 1960s, such as the unsuccessful Rockwell XFV-12, the F-35B is to be the first operational supersonic STOVL stealth fighter. The single-engine F-35 resembles the larger twin-engined Lockheed Martin F-22 Raptor, drawing design elements from it. The exhaust duct design was inspired by the General Dynamics Model 200, proposed for a 1972 supersonic VTOL fighter requirement for the Sea Control Ship.

 

Lockheed Martin has suggested that the F-35 could replace the USAF's F-15C/D fighters in the air-superiority role and the F-15E Strike Eagle in the ground-attack role. It has also stated the F-35 is intended to have close- and long-range air-to-air capability second only to that of the F-22 Raptor, and that the F-35 has an advantage over the F-22 in basing flexibility and possesses "advanced sensors and information fusion".

 

Testifying before the House Appropriations Committee on 25 March 2009, acquisition deputy to the assistant secretary of the Air Force, Lt. Gen. Mark D. "Shack" Shackelford, stated that the F-35 is designed to be America's "premier surface-to-air missile killer, and is uniquely equipped for this mission with cutting-edge processing power, synthetic aperture radar integration techniques, and advanced target recognition".

  

Improvements

 

Ostensible improvements over past-generation fighter aircraft include:

 

Durable, low-maintenance stealth technology, using structural fiber mat instead of the high-maintenance coatings of legacy stealth platforms.

 

Integrated avionics and sensor fusion that combine information from off- and on-board sensors to increase the pilot's situational awareness and improve target identification and weapon delivery, and to relay information quickly to other command and control (C2) nodes.

 

High-speed data networking including IEEE 1394b and Fibre Channel (Fibre Channel is also used on Boeing's Super Hornet.

 

The Autonomic Logistics Global Sustainment, Autonomic Logistics Information System (ALIS), and Computerized maintenance management system to help ensure the aircraft can remain operational with minimal maintenance manpower The Pentagon has moved to open up the competitive bidding by other companies. This was after Lockheed Martin stated that instead of costing 20% less than the F-16 per flight hour, the F-35 would actually cost 12% more. Though the ALGS is intended to reduce maintenance costs, the company disagrees with including the cost of this system in the aircraft ownership calculations. The USMC has implemented a workaround for a cyber vulnerability in the system. The ALIS system currently requires a shipping-container load of servers to run, but Lockheed is working on a more portable version to support the Marines' expeditionary operations.

 

Electro-hydrostatic actuators run by a power-by-wire flight-control system.

 

A modern and updated flight simulator, which may be used for a greater fraction of pilot training to reduce the costly flight hours of the actual aircraft.

 

Lightweight, powerful lithium-ion batteries to provide power to run the control surfaces in an emergency.

 

Structural composites in the F-35 are 35% of the airframe weight (up from 25% in the F-22). The majority of these are bismaleimide and composite epoxy materials. The F-35 will be the first mass-produced aircraft to include structural nanocomposites, namely carbon nanotube-reinforced epoxy. Experience of the F-22's problems with corrosion led to the F-35 using a gap filler that causes less galvanic corrosion to the airframe's skin, designed with fewer gaps requiring filler and implementing better drainage. The relatively short 35-foot wingspan of the A and B variants is set by the F-35B's requirement to fit inside the Navy's current amphibious assault ship parking area and elevators; the F-35C's longer wing is considered to be more fuel efficient.

  

Costs

 

A U.S. Navy study found that the F-35 will cost 30 to 40% more to maintain than current jet fighters, not accounting for inflation over the F-35's operational lifetime. A Pentagon study concluded a $1 trillion maintenance cost for the entire fleet over its lifespan, not accounting for inflation. The F-35 program office found that as of January 2014, costs for the F-35 fleet over a 53-year lifecycle was $857 billion. Costs for the fighter have been dropping and accounted for the 22 percent life cycle drop since 2010. Lockheed stated that by 2019, pricing for the fifth-generation aircraft will be less than fourth-generation fighters. An F-35A in 2019 is expected to cost $85 million per unit complete with engines and full mission systems, inflation adjusted from $75 million in December 2013.

The Lockheed Martin F-35A Lightning II "Joint Strike Fighter" sits in a hangar loaded with dummy external munitions, Feb. 13, 2019 at Luke Air Force Base, Ariz. After completing the external pylon installation training, the weapons loading standardization crew, a team of three Airmen, became the first team at Luke to be certified on external GBU-12 bomb and AIM-9 missile loading.

  

From Wikipedia, the free encyclopedia

 

The Lockheed Martin F-35 Lightning II is a family of single-seat, single-engine, all-weather, stealth, fifth-generation, multirole combat aircraft, designed for ground-attack and air-superiority missions. It is built by Lockheed Martin and many subcontractors, including Northrop Grumman, Pratt & Whitney, and BAE Systems.

 

The F-35 has three main models: the conventional takeoff and landing F-35A (CTOL), the short take-off and vertical-landing F-35B (STOVL), and the catapult-assisted take-off but arrested recovery, carrier-based F-35C (CATOBAR). The F-35 descends from the Lockheed Martin X-35, the design that was awarded the Joint Strike Fighter (JSF) program over the competing Boeing X-32. The official Lightning II name has proven deeply unpopular and USAF pilots have nicknamed it Panther, instead.

 

The United States principally funds F-35 development, with additional funding from other NATO members and close U.S. allies, including the United Kingdom, Italy, Australia, Canada, Norway, Denmark, the Netherlands, and formerly Turkey. These funders generally receive subcontracts to manufacture components for the aircraft; for example, Turkey was the sole supplier of several F-35 parts until its removal from the program in July 2019. Several other countries have ordered, or are considering ordering, the aircraft.

 

As the largest and most expensive military program ever, the F-35 became the subject of much scrutiny and criticism in the U.S. and in other countries. In 2013 and 2014, critics argued that the plane was "plagued with design flaws", with many blaming the procurement process in which Lockheed was allowed "to design, test, and produce the F-35 all at the same time," instead of identifying and fixing "defects before firing up its production line". By 2014, the program was "$163 billion over budget [and] seven years behind schedule". Critics also contend that the program's high sunk costs and political momentum make it "too big to kill".

 

The F-35 first flew on 15 December 2006. In July 2015, the United States Marines declared its first squadron of F-35B fighters ready for deployment. However, the DOD-based durability testing indicated the service life of early-production F-35B aircraft is well under the expected 8,000 flight hours, and may be as low as 2,100 flight hours. Lot 9 and later aircraft include design changes but service life testing has yet to occur. The U.S. Air Force declared its first squadron of F-35As ready for deployment in August 2016. The U.S. Navy declared its first F-35Cs ready in February 2019. In 2018, the F-35 made its combat debut with the Israeli Air Force.

 

The U.S. stated plan is to buy 2,663 F-35s, which will provide the bulk of the crewed tactical airpower of the U.S. Air Force, Navy, and Marine Corps in coming decades. Deliveries of the F-35 for the U.S. military are scheduled until 2037 with a projected service life up to 2070.

 

Development

 

F-35 development started in 1992 with the origins of the "Joint Strike Fighter" (JSF) program and was to culminate in full production by 2018. The X-35 first flew on 24 October 2000 and the F-35A on 15 December 2006.

 

The F-35 was developed to replace most US fighter jets with the variants of a single design that would be common to all branches of the military. It was developed in co-operation with a number of foreign partners, and, unlike the F-22 Raptor, intended to be available for export. Three variants were designed: the F-35A (CTOL), the F-35B (STOVL), and the F-35C (CATOBAR). Despite being intended to share most of their parts to reduce costs and improve maintenance logistics, by 2017, the effective commonality was only 20%. The program received considerable criticism for cost overruns during development and for the total projected cost of the program over the lifetime of the jets.

 

By 2017, the program was expected to cost $406.5 billion over its lifetime (i.e. until 2070) for acquisition of the jets, and an additional $1.1 trillion for operations and maintenance. A number of design deficiencies were alleged, such as: carrying a small internal payload; performance inferior to the aircraft being replaced, particularly the F-16; lack of safety in relying on a single engine; and flaws such as the vulnerability of the fuel tank to fire and the propensity for transonic roll-off (wing drop). The possible obsolescence of stealth technology was also criticized.

  

Design

 

Overview

 

Although several experimental designs have been developed since the 1960s, such as the unsuccessful Rockwell XFV-12, the F-35B is to be the first operational supersonic STOVL stealth fighter. The single-engine F-35 resembles the larger twin-engined Lockheed Martin F-22 Raptor, drawing design elements from it. The exhaust duct design was inspired by the General Dynamics Model 200, proposed for a 1972 supersonic VTOL fighter requirement for the Sea Control Ship.

 

Lockheed Martin has suggested that the F-35 could replace the USAF's F-15C/D fighters in the air-superiority role and the F-15E Strike Eagle in the ground-attack role. It has also stated the F-35 is intended to have close- and long-range air-to-air capability second only to that of the F-22 Raptor, and that the F-35 has an advantage over the F-22 in basing flexibility and possesses "advanced sensors and information fusion".

 

Testifying before the House Appropriations Committee on 25 March 2009, acquisition deputy to the assistant secretary of the Air Force, Lt. Gen. Mark D. "Shack" Shackelford, stated that the F-35 is designed to be America's "premier surface-to-air missile killer, and is uniquely equipped for this mission with cutting-edge processing power, synthetic aperture radar integration techniques, and advanced target recognition".

  

Improvements

 

Ostensible improvements over past-generation fighter aircraft include:

 

Durable, low-maintenance stealth technology, using structural fiber mat instead of the high-maintenance coatings of legacy stealth platforms.

 

Integrated avionics and sensor fusion that combine information from off- and on-board sensors to increase the pilot's situational awareness and improve target identification and weapon delivery, and to relay information quickly to other command and control (C2) nodes.

 

High-speed data networking including IEEE 1394b and Fibre Channel (Fibre Channel is also used on Boeing's Super Hornet.

 

The Autonomic Logistics Global Sustainment, Autonomic Logistics Information System (ALIS), and Computerized maintenance management system to help ensure the aircraft can remain operational with minimal maintenance manpower The Pentagon has moved to open up the competitive bidding by other companies. This was after Lockheed Martin stated that instead of costing 20% less than the F-16 per flight hour, the F-35 would actually cost 12% more. Though the ALGS is intended to reduce maintenance costs, the company disagrees with including the cost of this system in the aircraft ownership calculations. The USMC has implemented a workaround for a cyber vulnerability in the system. The ALIS system currently requires a shipping-container load of servers to run, but Lockheed is working on a more portable version to support the Marines' expeditionary operations.

 

Electro-hydrostatic actuators run by a power-by-wire flight-control system.

 

A modern and updated flight simulator, which may be used for a greater fraction of pilot training to reduce the costly flight hours of the actual aircraft.

 

Lightweight, powerful lithium-ion batteries to provide power to run the control surfaces in an emergency.

 

Structural composites in the F-35 are 35% of the airframe weight (up from 25% in the F-22). The majority of these are bismaleimide and composite epoxy materials. The F-35 will be the first mass-produced aircraft to include structural nanocomposites, namely carbon nanotube-reinforced epoxy. Experience of the F-22's problems with corrosion led to the F-35 using a gap filler that causes less galvanic corrosion to the airframe's skin, designed with fewer gaps requiring filler and implementing better drainage. The relatively short 35-foot wingspan of the A and B variants is set by the F-35B's requirement to fit inside the Navy's current amphibious assault ship parking area and elevators; the F-35C's longer wing is considered to be more fuel efficient.

  

Costs

 

A U.S. Navy study found that the F-35 will cost 30 to 40% more to maintain than current jet fighters, not accounting for inflation over the F-35's operational lifetime. A Pentagon study concluded a $1 trillion maintenance cost for the entire fleet over its lifespan, not accounting for inflation. The F-35 program office found that as of January 2014, costs for the F-35 fleet over a 53-year lifecycle was $857 billion. Costs for the fighter have been dropping and accounted for the 22 percent life cycle drop since 2010. Lockheed stated that by 2019, pricing for the fifth-generation aircraft will be less than fourth-generation fighters. An F-35A in 2019 is expected to cost $85 million per unit complete with engines and full mission systems, inflation adjusted from $75 million in December 2013.

Three Lockheed Martin F-35A Lighting II "Joint Strike Fighter's", assigned to the 63rd Fighter Squadron at Luke Air Force Base, Ariz., fly in formation during a refueling mission Aug. 27, 2019, near Phoenix. A Boeing KC-135 Stratotanker, assigned to the Arizona Air National Guard, 161st Fueling Wing, refueled six F-35s. During a refueling mission, the boom operator extends the boom to make contact with the aircraft and once in contact, fuel is pumped through the boom to the aircraft.

  

LUKE AIR FORCE BASE, Ariz. --

From start to finish, many Airmen contribute to the success of an F-35A Lightning II strike mission.

 

Mission success depends on a smooth transition from every required task from building bombs to maintaining the jets to flying them. For a strike mission, the whole process starts with building the munitions.

 

“There’s a lot of prep work that goes into building a munition,” said Staff Sgt. Noah Dankocsik, 56th Equipment Maintenance Squadron conventional maintenance crew chief. “It requires reading through multiple steps in our technical data to properly putting it together. To build munitions, you have to put on tails and noses, and you have the bomb body itself to prepare.”

 

Once munitions are built they are put on a trailer and the Airmen from the line delivery section pull the trailers of bombs to the flightline to transfer to the weapons load crews. Weapons then take those bombs and load them onto the jets, Dankocsik said.

 

In addition to having the weapons loaded, F-35s are inspected and prepped for flight.

 

“Our crew chiefs perform Before Operation Servicing (BOS) inspections to ensure aircraft are serviced and ready for flight,” said Master Sgt. Micheal Whitehead, 63rd Aircraft Maintenance Unit (AMU) F-35 lead production superintendent. “Crew chiefs, avionics, weapons, Autonomic Logistics Information System expediters will then review aircraft forms and clear any discrepancies. The production superintendent will perform a forms review and a walk around of the aircraft, (prior to) releasing it for flight.”

 

Recently, all the cohesion and cooperation between these units came together Aug. 27 during the ‘Panther Beast’ 63rd Fighter Squadron competition.

Competing pilots flew 50 miles to acquire and destroy 6 to 12 targets over a 45-minute period in hopes of becoming the winners of ‘Panther Beast’, said Lt. Col. Curtis Dougherty, 63rd Fighter Squadron commander.

 

“After landing, the tape review will reveal the truth, and we’ll celebrate the victors at a fighter squadron and aircraft maintenance unit awards ceremony,” said Dougherty.

 

Airmen from multiple units worked together to build the munitions used, maintain the aircraft and fly the jets. Dougherty said it was their cooperation that made the competition possible.

 

“The work started weeks before weapons hit targets,” he said. “Our AMU has been hard at work loading aircraft with external pylons that we’ve never flown with before at Luke. Ammo has spent countless hours building more weapons than we’ve ever dropped in this squadron’s history. The pilots have spent that time planning: determining which targets and attacks will challenge the squadron’s instructors and ensuring everyone has the knowledge requisite to succeed. On the day of the mission, it all comes together.”

 

While the competition is a special event, maintenance, ammo and pilots work together to perform these tasks frequently. Dougherty said, it’s this synergy that allows our Air Force to be an effective fighting force.

 

“To succeed, we rely on the world’s finest maintenance professionals to care about the small details so that all of the critical aircraft systems work at their peak capability and weapons function the way they were intended,” he added. “We ask our pilots to prepare and brief with diligence to be ready to execute at the highest levels. The team environment and esprit de corps that extends across our aircraft maintenance unit and fighter squadron inspires the finest our Airmen have to offer.”

  

From Wikipedia, the free encyclopedia

 

The Lockheed Martin F-35 Lightning II is a family of single-seat, single-engine, all-weather, stealth, fifth-generation, multirole combat aircraft, designed for ground-attack and air-superiority missions. It is built by Lockheed Martin and many subcontractors, including Northrop Grumman, Pratt & Whitney, and BAE Systems.

 

The F-35 has three main models: the conventional takeoff and landing F-35A (CTOL), the short take-off and vertical-landing F-35B (STOVL), and the catapult-assisted take-off but arrested recovery, carrier-based F-35C (CATOBAR). The F-35 descends from the Lockheed Martin X-35, the design that was awarded the Joint Strike Fighter (JSF) program over the competing Boeing X-32. The official Lightning II name has proven deeply unpopular and USAF pilots have nicknamed it Panther, instead.

 

The United States principally funds F-35 development, with additional funding from other NATO members and close U.S. allies, including the United Kingdom, Italy, Australia, Canada, Norway, Denmark, the Netherlands, and formerly Turkey. These funders generally receive subcontracts to manufacture components for the aircraft; for example, Turkey was the sole supplier of several F-35 parts until its removal from the program in July 2019. Several other countries have ordered, or are considering ordering, the aircraft.

 

As the largest and most expensive military program ever, the F-35 became the subject of much scrutiny and criticism in the U.S. and in other countries. In 2013 and 2014, critics argued that the plane was "plagued with design flaws", with many blaming the procurement process in which Lockheed was allowed "to design, test, and produce the F-35 all at the same time," instead of identifying and fixing "defects before firing up its production line". By 2014, the program was "$163 billion over budget [and] seven years behind schedule". Critics also contend that the program's high sunk costs and political momentum make it "too big to kill".

 

The F-35 first flew on 15 December 2006. In July 2015, the United States Marines declared its first squadron of F-35B fighters ready for deployment. However, the DOD-based durability testing indicated the service life of early-production F-35B aircraft is well under the expected 8,000 flight hours, and may be as low as 2,100 flight hours. Lot 9 and later aircraft include design changes but service life testing has yet to occur. The U.S. Air Force declared its first squadron of F-35As ready for deployment in August 2016. The U.S. Navy declared its first F-35Cs ready in February 2019. In 2018, the F-35 made its combat debut with the Israeli Air Force.

 

The U.S. stated plan is to buy 2,663 F-35s, which will provide the bulk of the crewed tactical airpower of the U.S. Air Force, Navy, and Marine Corps in coming decades. Deliveries of the F-35 for the U.S. military are scheduled until 2037 with a projected service life up to 2070.

 

Development

 

F-35 development started in 1992 with the origins of the "Joint Strike Fighter" (JSF) program and was to culminate in full production by 2018. The X-35 first flew on 24 October 2000 and the F-35A on 15 December 2006.

 

The F-35 was developed to replace most US fighter jets with the variants of a single design that would be common to all branches of the military. It was developed in co-operation with a number of foreign partners, and, unlike the F-22 Raptor, intended to be available for export. Three variants were designed: the F-35A (CTOL), the F-35B (STOVL), and the F-35C (CATOBAR). Despite being intended to share most of their parts to reduce costs and improve maintenance logistics, by 2017, the effective commonality was only 20%. The program received considerable criticism for cost overruns during development and for the total projected cost of the program over the lifetime of the jets.

 

By 2017, the program was expected to cost $406.5 billion over its lifetime (i.e. until 2070) for acquisition of the jets, and an additional $1.1 trillion for operations and maintenance. A number of design deficiencies were alleged, such as: carrying a small internal payload; performance inferior to the aircraft being replaced, particularly the F-16; lack of safety in relying on a single engine; and flaws such as the vulnerability of the fuel tank to fire and the propensity for transonic roll-off (wing drop). The possible obsolescence of stealth technology was also criticized.

  

Design

 

Overview

 

Although several experimental designs have been developed since the 1960s, such as the unsuccessful Rockwell XFV-12, the F-35B is to be the first operational supersonic STOVL stealth fighter. The single-engine F-35 resembles the larger twin-engined Lockheed Martin F-22 Raptor, drawing design elements from it. The exhaust duct design was inspired by the General Dynamics Model 200, proposed for a 1972 supersonic VTOL fighter requirement for the Sea Control Ship.

 

Lockheed Martin has suggested that the F-35 could replace the USAF's F-15C/D fighters in the air-superiority role and the F-15E Strike Eagle in the ground-attack role. It has also stated the F-35 is intended to have close- and long-range air-to-air capability second only to that of the F-22 Raptor, and that the F-35 has an advantage over the F-22 in basing flexibility and possesses "advanced sensors and information fusion".

 

Testifying before the House Appropriations Committee on 25 March 2009, acquisition deputy to the assistant secretary of the Air Force, Lt. Gen. Mark D. "Shack" Shackelford, stated that the F-35 is designed to be America's "premier surface-to-air missile killer, and is uniquely equipped for this mission with cutting-edge processing power, synthetic aperture radar integration techniques, and advanced target recognition".

  

Improvements

 

Ostensible improvements over past-generation fighter aircraft include:

 

Durable, low-maintenance stealth technology, using structural fiber mat instead of the high-maintenance coatings of legacy stealth platforms.

 

Integrated avionics and sensor fusion that combine information from off- and on-board sensors to increase the pilot's situational awareness and improve target identification and weapon delivery, and to relay information quickly to other command and control (C2) nodes.

 

High-speed data networking including IEEE 1394b and Fibre Channel (Fibre Channel is also used on Boeing's Super Hornet.

 

The Autonomic Logistics Global Sustainment, Autonomic Logistics Information System (ALIS), and Computerized maintenance management system to help ensure the aircraft can remain operational with minimal maintenance manpower The Pentagon has moved to open up the competitive bidding by other companies. This was after Lockheed Martin stated that instead of costing 20% less than the F-16 per flight hour, the F-35 would actually cost 12% more. Though the ALGS is intended to reduce maintenance costs, the company disagrees with including the cost of this system in the aircraft ownership calculations. The USMC has implemented a workaround for a cyber vulnerability in the system. The ALIS system currently requires a shipping-container load of servers to run, but Lockheed is working on a more portable version to support the Marines' expeditionary operations.

 

Electro-hydrostatic actuators run by a power-by-wire flight-control system.

 

A modern and updated flight simulator, which may be used for a greater fraction of pilot training to reduce the costly flight hours of the actual aircraft.

 

Lightweight, powerful lithium-ion batteries to provide power to run the control surfaces in an emergency.

 

Structural composites in the F-35 are 35% of the airframe weight (up from 25% in the F-22). The majority of these are bismaleimide and composite epoxy materials. The F-35 will be the first mass-produced aircraft to include structural nanocomposites, namely carbon nanotube-reinforced epoxy. Experience of the F-22's problems with corrosion led to the F-35 using a gap filler that causes less galvanic corrosion to the airframe's skin, designed with fewer gaps requiring filler and implementing better drainage. The relatively short 35-foot wingspan of the A and B variants is set by the F-35B's requirement to fit inside the Navy's current amphibious assault ship parking area and elevators; the F-35C's longer wing is considered to be more fuel efficient.

  

Costs

 

A U.S. Navy study found that the F-35 will cost 30 to 40% more to maintain than current jet fighters, not accounting for inflation over the F-35's operational lifetime. A Pentagon study concluded a $1 trillion maintenance cost for the entire fleet over its lifespan, not accounting for inflation. The F-35 program office found that as of January 2014, costs for the F-35 fleet over a 53-year lifecycle was $857 billion. Costs for the fighter have been dropping and accounted for the 22 percent life cycle drop since 2010. Lockheed stated that by 2019, pricing for the fifth-generation aircraft will be less than fourth-generation fighters. An F-35A in 2019 is expected to cost $85 million per unit complete with engines and full mission systems, inflation adjusted from $75 million in December 2013.

Credit to VoodoKR for the technique behind making the wheels.

 

In 1999, Kongo Firearms Incorporated developed the Third-track Artillery Vehicle, a modular unit capable of carrying a wide variety of weapon loadouts, although it was designed specifically to carry artillery onto the battlefield.

The TAV is moderately armored, although it is mine-proof, and is also kitted out with KFI's Armored Vehicle Protection System, which fires a variety of smoke grenades and infra red screening rounds, as well as anti-personnel grenades.

Any artillery that the TAV happens to be carrying can be connected to the onboard computer, which requires only a single operator. For this reason, the minimum crew is 2; one driver and one artillery operator. However, the TAV can seat up to four, which allows for communications specialists, officers, and mechanics to also be present when and if the need arises.

The model shown here is fitted with the Python Multiple Launching Rocket System, which shoots up to 40 rockets at a time from the multiple barreled pod. Because of the computerized auto-loader, it has a relatively fast rate of fire, up to 2 rounds/second, and has a maximum range of 45 km. There is a wide variety of warheads available that can be mounted on the rockets, including but not limited to: incendiary, high explosive, submunition anti-personnel, biochemical, and vision-obscuring.

A Royal Australian Air Force Lockheed Martin F-35A Lightning II "Joint Strike Fighter" taxis at Luke Air Force Base, Ariz., Dec. 3, 2018. Two F-35s were preparing to take off and fly to Hawaii as part of their multi-day journey to Australia.

 

To RAF as A 36-009

  

From Wikipedia, the free encyclopedia

 

The Lockheed Martin F-35 Lightning II is a family of single-seat, single-engine, all-weather, stealth, fifth-generation, multirole combat aircraft, designed for ground-attack and air-superiority missions. It is built by Lockheed Martin and many subcontractors, including Northrop Grumman, Pratt & Whitney, and BAE Systems.

 

The F-35 has three main models: the conventional takeoff and landing F-35A (CTOL), the short take-off and vertical-landing F-35B (STOVL), and the catapult-assisted take-off but arrested recovery, carrier-based F-35C (CATOBAR). The F-35 descends from the Lockheed Martin X-35, the design that was awarded the Joint Strike Fighter (JSF) program over the competing Boeing X-32. The official Lightning II name has proven deeply unpopular and USAF pilots have nicknamed it Panther, instead.

 

The United States principally funds F-35 development, with additional funding from other NATO members and close U.S. allies, including the United Kingdom, Italy, Australia, Canada, Norway, Denmark, the Netherlands, and formerly Turkey. These funders generally receive subcontracts to manufacture components for the aircraft; for example, Turkey was the sole supplier of several F-35 parts until its removal from the program in July 2019. Several other countries have ordered, or are considering ordering, the aircraft.

 

As the largest and most expensive military program ever, the F-35 became the subject of much scrutiny and criticism in the U.S. and in other countries. In 2013 and 2014, critics argued that the plane was "plagued with design flaws", with many blaming the procurement process in which Lockheed was allowed "to design, test, and produce the F-35 all at the same time," instead of identifying and fixing "defects before firing up its production line". By 2014, the program was "$163 billion over budget [and] seven years behind schedule". Critics also contend that the program's high sunk costs and political momentum make it "too big to kill".

 

The F-35 first flew on 15 December 2006. In July 2015, the United States Marines declared its first squadron of F-35B fighters ready for deployment. However, the DOD-based durability testing indicated the service life of early-production F-35B aircraft is well under the expected 8,000 flight hours, and may be as low as 2,100 flight hours. Lot 9 and later aircraft include design changes but service life testing has yet to occur. The U.S. Air Force declared its first squadron of F-35As ready for deployment in August 2016. The U.S. Navy declared its first F-35Cs ready in February 2019. In 2018, the F-35 made its combat debut with the Israeli Air Force.

 

The U.S. stated plan is to buy 2,663 F-35s, which will provide the bulk of the crewed tactical airpower of the U.S. Air Force, Navy, and Marine Corps in coming decades. Deliveries of the F-35 for the U.S. military are scheduled until 2037 with a projected service life up to 2070.

 

Development

 

F-35 development started in 1992 with the origins of the "Joint Strike Fighter" (JSF) program and was to culminate in full production by 2018. The X-35 first flew on 24 October 2000 and the F-35A on 15 December 2006.

 

The F-35 was developed to replace most US fighter jets with the variants of a single design that would be common to all branches of the military. It was developed in co-operation with a number of foreign partners, and, unlike the F-22 Raptor, intended to be available for export. Three variants were designed: the F-35A (CTOL), the F-35B (STOVL), and the F-35C (CATOBAR). Despite being intended to share most of their parts to reduce costs and improve maintenance logistics, by 2017, the effective commonality was only 20%. The program received considerable criticism for cost overruns during development and for the total projected cost of the program over the lifetime of the jets.

 

By 2017, the program was expected to cost $406.5 billion over its lifetime (i.e. until 2070) for acquisition of the jets, and an additional $1.1 trillion for operations and maintenance. A number of design deficiencies were alleged, such as: carrying a small internal payload; performance inferior to the aircraft being replaced, particularly the F-16; lack of safety in relying on a single engine; and flaws such as the vulnerability of the fuel tank to fire and the propensity for transonic roll-off (wing drop). The possible obsolescence of stealth technology was also criticized.

  

Design

 

Overview

 

Although several experimental designs have been developed since the 1960s, such as the unsuccessful Rockwell XFV-12, the F-35B is to be the first operational supersonic STOVL stealth fighter. The single-engine F-35 resembles the larger twin-engined Lockheed Martin F-22 Raptor, drawing design elements from it. The exhaust duct design was inspired by the General Dynamics Model 200, proposed for a 1972 supersonic VTOL fighter requirement for the Sea Control Ship.

 

Lockheed Martin has suggested that the F-35 could replace the USAF's F-15C/D fighters in the air-superiority role and the F-15E Strike Eagle in the ground-attack role. It has also stated the F-35 is intended to have close- and long-range air-to-air capability second only to that of the F-22 Raptor, and that the F-35 has an advantage over the F-22 in basing flexibility and possesses "advanced sensors and information fusion".

 

Testifying before the House Appropriations Committee on 25 March 2009, acquisition deputy to the assistant secretary of the Air Force, Lt. Gen. Mark D. "Shack" Shackelford, stated that the F-35 is designed to be America's "premier surface-to-air missile killer, and is uniquely equipped for this mission with cutting-edge processing power, synthetic aperture radar integration techniques, and advanced target recognition".

  

Improvements

 

Ostensible improvements over past-generation fighter aircraft include:

 

Durable, low-maintenance stealth technology, using structural fiber mat instead of the high-maintenance coatings of legacy stealth platforms.

 

Integrated avionics and sensor fusion that combine information from off- and on-board sensors to increase the pilot's situational awareness and improve target identification and weapon delivery, and to relay information quickly to other command and control (C2) nodes.

 

High-speed data networking including IEEE 1394b and Fibre Channel (Fibre Channel is also used on Boeing's Super Hornet.

 

The Autonomic Logistics Global Sustainment, Autonomic Logistics Information System (ALIS), and Computerized maintenance management system to help ensure the aircraft can remain operational with minimal maintenance manpower The Pentagon has moved to open up the competitive bidding by other companies. This was after Lockheed Martin stated that instead of costing 20% less than the F-16 per flight hour, the F-35 would actually cost 12% more. Though the ALGS is intended to reduce maintenance costs, the company disagrees with including the cost of this system in the aircraft ownership calculations. The USMC has implemented a workaround for a cyber vulnerability in the system. The ALIS system currently requires a shipping-container load of servers to run, but Lockheed is working on a more portable version to support the Marines' expeditionary operations.

 

Electro-hydrostatic actuators run by a power-by-wire flight-control system.

 

A modern and updated flight simulator, which may be used for a greater fraction of pilot training to reduce the costly flight hours of the actual aircraft.

 

Lightweight, powerful lithium-ion batteries to provide power to run the control surfaces in an emergency.

 

Structural composites in the F-35 are 35% of the airframe weight (up from 25% in the F-22). The majority of these are bismaleimide and composite epoxy materials. The F-35 will be the first mass-produced aircraft to include structural nanocomposites, namely carbon nanotube-reinforced epoxy. Experience of the F-22's problems with corrosion led to the F-35 using a gap filler that causes less galvanic corrosion to the airframe's skin, designed with fewer gaps requiring filler and implementing better drainage. The relatively short 35-foot wingspan of the A and B variants is set by the F-35B's requirement to fit inside the Navy's current amphibious assault ship parking area and elevators; the F-35C's longer wing is considered to be more fuel efficient.

  

Costs

 

A U.S. Navy study found that the F-35 will cost 30 to 40% more to maintain than current jet fighters, not accounting for inflation over the F-35's operational lifetime. A Pentagon study concluded a $1 trillion maintenance cost for the entire fleet over its lifespan, not accounting for inflation. The F-35 program office found that as of January 2014, costs for the F-35 fleet over a 53-year lifecycle was $857 billion. Costs for the fighter have been dropping and accounted for the 22 percent life cycle drop since 2010. Lockheed stated that by 2019, pricing for the fifth-generation aircraft will be less than fourth-generation fighters. An F-35A in 2019 is expected to cost $85 million per unit complete with engines and full mission systems, inflation adjusted from $75 million in December 2013.

U.S. Air Force 1st Lt. David Moore, a Lockheed Martin F-35A "Lightning II" pilot from the 34th Fighter Squadron, climbs out of the cockpit after a flight from Hill Air Force Base, Utah, to Joint Base Pearl Harbor-Hickam, Hawaii, Oct. 30, 2017. A dozen F-35As and approximately 300 Airmen are on their way to Kadena Air Base, Japan, deployed under U.S. Pacific Command's (PACOM) Theater Security Package program, which has been in operation since 2004. This marks PACOM’s first operational tasking for the F-35A and builds upon the successful debut of the fifth-generation stealth fighter in the Indo-Asia-Pacific region at the Seoul International Aerospace & Defense Exhibition earlier this month.

  

From Wikipedia, the free encyclopedia

 

The Lockheed Martin F-35 "Lightning II" is a family of single-seat, single-engine, all-weather, stealth, fifth-generation, multirole combat aircraft, designed for ground-attack and air-superiority missions. It is built by Lockheed Martin and many subcontractors, including Northrop Grumman, Pratt & Whitney, and BAE Systems.

 

The F-35 has three main models: the conventional takeoff and landing F-35A (CTOL), the short take-off and vertical-landing F-35B (STOVL), and the catapult-assisted take-off but arrested recovery, carrier-based F-35C (CATOBAR). The F-35 descends from the Lockheed Martin X-35, the design that was awarded the "Joint Strike Fighter" (JSF) program over the competing Boeing X-32. The official "Lightning II" name has proven deeply unpopular and USAF pilots have nicknamed it Panther, instead.

 

The United States principally funds F-35 development, with additional funding from other NATO members and close U.S. allies, including the United Kingdom, Italy, Australia, Canada, Norway, Denmark, the Netherlands, and formerly Turkey. These funders generally receive subcontracts to manufacture components for the aircraft; for example, Turkey was the sole supplier of several F-35 parts until its removal from the program in July 2019. Several other countries have ordered, or are considering ordering, the aircraft.

 

As the largest and most expensive military program ever, the F-35 became the subject of much scrutiny and criticism in the U.S. and in other countries. In 2013 and 2014, critics argued that the plane was "plagued with design flaws", with many blaming the procurement process in which Lockheed was allowed "to design, test, and produce the F-35 all at the same time," instead of identifying and fixing "defects before firing up its production line". By 2014, the program was "$163 billion over budget [and] seven years behind schedule". Critics also contend that the program's high sunk costs and political momentum make it "too big to kill".

 

The F-35 first flew on 15 December 2006. In July 2015, the United States Marines declared its first squadron of F-35B fighters ready for deployment. However, the DOD-based durability testing indicated the service life of early-production F-35B aircraft is well under the expected 8,000 flight hours, and may be as low as 2,100 flight hours. Lot 9 and later aircraft include design changes but service life testing has yet to occur. The U.S. Air Force declared its first squadron of F-35As ready for deployment in August 2016. The U.S. Navy declared its first F-35Cs ready in February 2019. In 2018, the F-35 made its combat debut with the Israeli Air Force.

 

The U.S. stated plan is to buy 2,663 F-35s, which will provide the bulk of the crewed tactical airpower of the U.S. Air Force, Navy, and Marine Corps in coming decades. Deliveries of the F-35 for the U.S. military are scheduled until 2037 with a projected service life up to 2070.

 

Development

 

F-35 development started in 1992 with the origins of the "Joint Strike Fighter" (JSF) program and was to culminate in full production by 2018. The X-35 first flew on 24 October 2000 and the F-35A on 15 December 2006.

 

The F-35 was developed to replace most US fighter jets with the variants of a single design that would be common to all branches of the military. It was developed in co-operation with a number of foreign partners, and, unlike the F-22 "Raptor", intended to be available for export. Three variants were designed: the F-35A (CTOL), the F-35B (STOVL), and the F-35C (CATOBAR). Despite being intended to share most of their parts to reduce costs and improve maintenance logistics, by 2017, the effective commonality was only 20%. The program received considerable criticism for cost overruns during development and for the total projected cost of the program over the lifetime of the jets.

 

By 2017, the program was expected to cost $406.5 billion over its lifetime (i.e. until 2070) for acquisition of the jets, and an additional $1.1 trillion for operations and maintenance. A number of design deficiencies were alleged, such as: carrying a small internal payload; performance inferior to the aircraft being replaced, particularly the F-16; lack of safety in relying on a single engine; and flaws such as the vulnerability of the fuel tank to fire and the propensity for transonic roll-off (wing drop). The possible obsolescence of stealth technology was also criticized.

  

Design

 

Overview

 

Although several experimental designs have been developed since the 1960s, such as the unsuccessful Rockwell XFV-12, the F-35B is to be the first operational supersonic STOVL stealth fighter. The single-engine F-35 resembles the larger twin-engined Lockheed Martin F-22 "Raptor", drawing design elements from it. The exhaust duct design was inspired by the General Dynamics Model 200, proposed for a 1972 supersonic VTOL fighter requirement for the Sea Control Ship.

 

Lockheed Martin has suggested that the F-35 could replace the USAF's F-15C/D fighters in the air-superiority role and the F-15E "Strike Eagle" in the ground-attack role. It has also stated the F-35 is intended to have close- and long-range air-to-air capability second only to that of the F-22 "Raptor", and that the F-35 has an advantage over the F-22 in basing flexibility and possesses "advanced sensors and information fusion".

 

Testifying before the House Appropriations Committee on 25 March 2009, acquisition deputy to the assistant secretary of the Air Force, Lt. Gen. Mark D. "Shack" Shackelford, stated that the F-35 is designed to be America's "premier surface-to-air missile killer, and is uniquely equipped for this mission with cutting-edge processing power, synthetic aperture radar integration techniques, and advanced target recognition".

 

Improvements

Ostensible improvements over past-generation fighter aircraft include:

 

Durable, low-maintenance stealth technology, using structural fiber mat instead of the high-maintenance coatings of legacy stealth platforms.

Integrated avionics and sensor fusion that combine information from off- and on-board sensors to increase the pilot's situational awareness and improve target identification and weapon delivery, and to relay information quickly to other command and control (C2) nodes.

High-speed data networking including IEEE 1394b and Fibre Channel (Fibre Channel is also used on Boeing's "Super Hornet".

The Autonomic Logistics Global Sustainment, Autonomic Logistics Information System (ALIS), and Computerized maintenance management system to help ensure the aircraft can remain operational with minimal maintenance manpower The Pentagon has moved to open up the competitive bidding by other companies. This was after Lockheed Martin stated that instead of costing 20% less than the F-16 per flight hour, the F-35 would actually cost 12% more. Though the ALGS is intended to reduce maintenance costs, the company disagrees with including the cost of this system in the aircraft ownership calculations. The USMC has implemented a workaround for a cyber vulnerability in the system. The ALIS system currently requires a shipping-container load of servers to run, but Lockheed is working on a more portable version to support the Marines' expeditionary operations.

Electro-hydrostatic actuators run by a power-by-wire flight-control system.

A modern and updated flight simulator, which may be used for a greater fraction of pilot training to reduce the costly flight hours of the actual aircraft.

Lightweight, powerful lithium-ion batteries to provide power to run the control surfaces in an emergency.

Structural composites in the F-35 are 35% of the airframe weight (up from 25% in the F-22). The majority of these are bismaleimide and composite epoxy materials. The F-35 will be the first mass-produced aircraft to include structural nanocomposites, namely carbon nanotube-reinforced epoxy. Experience of the F-22's problems with corrosion led to the F-35 using a gap filler that causes less galvanic corrosion to the airframe's skin, designed with fewer gaps requiring filler and implementing better drainage. The relatively short 35-foot wingspan of the A and B variants is set by the F-35B's requirement to fit inside the Navy's current amphibious assault ship parking area and elevators; the F-35C's longer wing is considered to be more fuel efficient.

 

Costs

A U.S. Navy study found that the F-35 will cost 30 to 40% more to maintain than current jet fighters, not accounting for inflation over the F-35's operational lifetime. A Pentagon study concluded a $1 trillion maintenance cost for the entire fleet over its lifespan, not accounting for inflation. The F-35 program office found that as of January 2014, costs for the F-35 fleet over a 53-year lifecycle was $857 billion. Costs for the fighter have been dropping and accounted for the 22 percent life cycle drop since 2010. Lockheed stated that by 2019, pricing for the fifth-generation aircraft will be less than fourth-generation fighters. An F-35A in 2019 is expected to cost $85 million per unit complete with engines and full mission systems, inflation adjusted from $75 million in December 2013.

NELLIS AIR FORCE BASE, Nev. - Marines with Marine Fighter Attack Squadron (VMFA) 211 'Wake Island Avengers,' 3rd Marine Aircraft Wing, tow a Lockheed Martin F-35B "Lightning II" into a hangar for maintenance at Nellis Air Force Base, Nev., July 10. A total of 10 aircraft and more than 250 Marines with VMFA 211 will participate in Red Flag 17-3, a realistic combat training exercise hosted by the U.S. Air Force to assess the squadron’s ability to deploy and support contingency operations using the F-35B.

  

From Wikipedia, the free encyclopedia

 

The Lockheed Martin F-35 "Lightning II" is a family of single-seat, single-engine, all-weather, stealth, fifth-generation, multirole combat aircraft, designed for ground-attack and air-superiority missions. It is built by Lockheed Martin and many subcontractors, including Northrop Grumman, Pratt & Whitney, and BAE Systems.

 

The F-35 has three main models: the conventional takeoff and landing F-35A (CTOL), the short take-off and vertical-landing F-35B (STOVL), and the catapult-assisted take-off but arrested recovery, carrier-based F-35C (CATOBAR). The F-35 descends from the Lockheed Martin X-35, the design that was awarded the Joint Strike Fighter (JSF) program over the competing Boeing X-32. The official "Lightning II" name has proven deeply unpopular and USAF pilots have nicknamed it "Panther", instead.

 

The United States principally funds F-35 development, with additional funding from other NATO members and close U.S. allies, including the United Kingdom, Italy, Australia, Canada, Norway, Denmark, the Netherlands, and formerly Turkey. These funders generally receive subcontracts to manufacture components for the aircraft; for example, Turkey was the sole supplier of several F-35 parts until its removal from the program in July 2019. Several other countries have ordered, or are considering ordering, the aircraft.

 

As the largest and most expensive military program ever, the F-35 became the subject of much scrutiny and criticism in the U.S. and in other countries. In 2013 and 2014, critics argued that the plane was "plagued with design flaws", with many blaming the procurement process in which Lockheed was allowed "to design, test, and produce the F-35 all at the same time," instead of identifying and fixing "defects before firing up its production line". By 2014, the program was "$163 billion over budget [and] seven years behind schedule". Critics also contend that the program's high sunk costs and political momentum make it "too big to kill".

 

The F-35 first flew on 15 December 2006. In July 2015, the United States Marines declared its first squadron of F-35B fighters ready for deployment. However, the DOD-based durability testing indicated the service life of early-production F-35B aircraft is well under the expected 8,000 flight hours, and may be as low as 2,100 flight hours. Lot 9 and later aircraft include design changes but service life testing has yet to occur. The U.S. Air Force declared its first squadron of F-35As ready for deployment in August 2016. The U.S. Navy declared its first F-35Cs ready in February 2019. In 2018, the F-35 made its combat debut with the Israeli Air Force.

 

The U.S. stated plan is to buy 2,663 F-35s, which will provide the bulk of the crewed tactical airpower of the U.S. Air Force, Navy, and Marine Corps in coming decades. Deliveries of the F-35 for the U.S. military are scheduled until 2037 with a projected service life up to 2070.

 

Development

 

F-35 development started in 1992 with the origins of the "Joint Strike Fighter" (JSF) program and was to culminate in full production by 2018. The X-35 first flew on 24 October 2000 and the F-35A on 15 December 2006.

 

The F-35 was developed to replace most US fighter jets with the variants of a single design that would be common to all branches of the military. It was developed in co-operation with a number of foreign partners, and, unlike the F-22 "Raptor", intended to be available for export. Three variants were designed: the F-35A (CTOL), the F-35B (STOVL), and the F-35C (CATOBAR). Despite being intended to share most of their parts to reduce costs and improve maintenance logistics, by 2017, the effective commonality was only 20%. The program received considerable criticism for cost overruns during development and for the total projected cost of the program over the lifetime of the jets.

 

By 2017, the program was expected to cost $406.5 billion over its lifetime (i.e. until 2070) for acquisition of the jets, and an additional $1.1 trillion for operations and maintenance. A number of design deficiencies were alleged, such as: carrying a small internal payload; performance inferior to the aircraft being replaced, particularly the F-16; lack of safety in relying on a single engine; and flaws such as the vulnerability of the fuel tank to fire and the propensity for transonic roll-off (wing drop). The possible obsolescence of stealth technology was also criticized.

  

Design

 

Overview

 

Although several experimental designs have been developed since the 1960s, such as the unsuccessful Rockwell XFV-12, the F-35B is to be the first operational supersonic STOVL stealth fighter. The single-engine F-35 resembles the larger twin-engined Lockheed Martin F-22 "Raptor", drawing design elements from it. The exhaust duct design was inspired by the General Dynamics Model 200, proposed for a 1972 supersonic VTOL fighter requirement for the Sea Control Ship.

 

Lockheed Martin has suggested that the F-35 could replace the USAF's F-15C/D fighters in the air-superiority role and the F-15E "Strike Eagle" in the ground-attack role. It has also stated the F-35 is intended to have close- and long-range air-to-air capability second only to that of the F-22 "Raptor", and that the F-35 has an advantage over the F-22 in basing flexibility and possesses "advanced sensors and information fusion".

 

Testifying before the House Appropriations Committee on 25 March 2009, acquisition deputy to the assistant secretary of the Air Force, Lt. Gen. Mark D. "Shack" Shackelford, stated that the F-35 is designed to be America's "premier surface-to-air missile killer, and is uniquely equipped for this mission with cutting-edge processing power, synthetic aperture radar integration techniques, and advanced target recognition".

  

Improvements

 

Ostensible improvements over past-generation fighter aircraft include:

 

Durable, low-maintenance stealth technology, using structural fiber mat instead of the high-maintenance coatings of legacy stealth platforms.

 

Integrated avionics and sensor fusion that combine information from off- and on-board sensors to increase the pilot's situational awareness and improve target identification and weapon delivery, and to relay information quickly to other command and control (C2) nodes.

 

High-speed data networking including IEEE 1394b and Fibre Channel (Fibre Channel is also used on Boeing's "Super Hornet".

 

The Autonomic Logistics Global Sustainment, Autonomic Logistics Information System (ALIS), and Computerized maintenance management system to help ensure the aircraft can remain operational with minimal maintenance manpower The Pentagon has moved to open up the competitive bidding by other companies. This was after Lockheed Martin stated that instead of costing 20% less than the F-16 per flight hour, the F-35 would actually cost 12% more. Though the ALGS is intended to reduce maintenance costs, the company disagrees with including the cost of this system in the aircraft ownership calculations. The USMC has implemented a workaround for a cyber vulnerability in the system. The ALIS system currently requires a shipping-container load of servers to run, but Lockheed is working on a more portable version to support the Marines' expeditionary operations.

 

Electro-hydrostatic actuators run by a power-by-wire flight-control system.

 

A modern and updated flight simulator, which may be used for a greater fraction of pilot training to reduce the costly flight hours of the actual aircraft.

 

Lightweight, powerful lithium-ion batteries to provide power to run the control surfaces in an emergency.

 

Structural composites in the F-35 are 35% of the airframe weight (up from 25% in the F-22). The majority of these are bismaleimide and composite epoxy materials. The F-35 will be the first mass-produced aircraft to include structural nanocomposites, namely carbon nanotube-reinforced epoxy. Experience of the F-22's problems with corrosion led to the F-35 using a gap filler that causes less galvanic corrosion to the airframe's skin, designed with fewer gaps requiring filler and implementing better drainage. The relatively short 35-foot wingspan of the A and B variants is set by the F-35B's requirement to fit inside the Navy's current amphibious assault ship parking area and elevators; the F-35C's longer wing is considered to be more fuel efficient.

  

Costs

 

A U.S. Navy study found that the F-35 will cost 30 to 40% more to maintain than current jet fighters, not accounting for inflation over the F-35's operational lifetime. A Pentagon study concluded a $1 trillion maintenance cost for the entire fleet over its lifespan, not accounting for inflation. The F-35 program office found that as of January 2014, costs for the F-35 fleet over a 53-year lifecycle was $857 billion. Costs for the fighter have been dropping and accounted for the 22 percent life cycle drop since 2010. Lockheed stated that by 2019, pricing for the fifth-generation aircraft will be less than fourth-generation fighters. An F-35A in 2019 is expected to cost $85 million per unit complete with engines and full mission systems, inflation adjusted from $75 million in December 2013.

NELLIS AIR FORCE BASE, Nev. - Marines with Marine Fighter Attack Squadron (VMFA) 211 'Wake Island Avengers,' 3rd Marine Aircraft Wing, tow a Lockheed Martin F-35B "Lightning II" into a hangar for maintenance at Nellis Air Force Base, Nev., July 10. A total of 10 aircraft and more than 250 Marines with VMFA 211 will participate in Red Flag 17-3, a realistic combat training exercise hosted by the U.S. Air Force to assess the squadron’s ability to deploy and support contingency operations using the F-35B.

  

From Wikipedia, the free encyclopedia

 

The Lockheed Martin F-35 "Lightning II" is a family of single-seat, single-engine, all-weather, stealth, fifth-generation, multirole combat aircraft, designed for ground-attack and air-superiority missions. It is built by Lockheed Martin and many subcontractors, including Northrop Grumman, Pratt & Whitney, and BAE Systems.

 

The F-35 has three main models: the conventional takeoff and landing F-35A (CTOL), the short take-off and vertical-landing F-35B (STOVL), and the catapult-assisted take-off but arrested recovery, carrier-based F-35C (CATOBAR). The F-35 descends from the Lockheed Martin X-35, the design that was awarded the Joint Strike Fighter (JSF) program over the competing Boeing X-32. The official "Lightning II" name has proven deeply unpopular and USAF pilots have nicknamed it "Panther", instead.

 

The United States principally funds F-35 development, with additional funding from other NATO members and close U.S. allies, including the United Kingdom, Italy, Australia, Canada, Norway, Denmark, the Netherlands, and formerly Turkey. These funders generally receive subcontracts to manufacture components for the aircraft; for example, Turkey was the sole supplier of several F-35 parts until its removal from the program in July 2019. Several other countries have ordered, or are considering ordering, the aircraft.

 

As the largest and most expensive military program ever, the F-35 became the subject of much scrutiny and criticism in the U.S. and in other countries. In 2013 and 2014, critics argued that the plane was "plagued with design flaws", with many blaming the procurement process in which Lockheed was allowed "to design, test, and produce the F-35 all at the same time," instead of identifying and fixing "defects before firing up its production line". By 2014, the program was "$163 billion over budget [and] seven years behind schedule". Critics also contend that the program's high sunk costs and political momentum make it "too big to kill".

 

The F-35 first flew on 15 December 2006. In July 2015, the United States Marines declared its first squadron of F-35B fighters ready for deployment. However, the DOD-based durability testing indicated the service life of early-production F-35B aircraft is well under the expected 8,000 flight hours, and may be as low as 2,100 flight hours. Lot 9 and later aircraft include design changes but service life testing has yet to occur. The U.S. Air Force declared its first squadron of F-35As ready for deployment in August 2016. The U.S. Navy declared its first F-35Cs ready in February 2019. In 2018, the F-35 made its combat debut with the Israeli Air Force.

 

The U.S. stated plan is to buy 2,663 F-35s, which will provide the bulk of the crewed tactical airpower of the U.S. Air Force, Navy, and Marine Corps in coming decades. Deliveries of the F-35 for the U.S. military are scheduled until 2037 with a projected service life up to 2070.

 

Development

 

F-35 development started in 1992 with the origins of the "Joint Strike Fighter" (JSF) program and was to culminate in full production by 2018. The X-35 first flew on 24 October 2000 and the F-35A on 15 December 2006.

 

The F-35 was developed to replace most US fighter jets with the variants of a single design that would be common to all branches of the military. It was developed in co-operation with a number of foreign partners, and, unlike the F-22 "Raptor", intended to be available for export. Three variants were designed: the F-35A (CTOL), the F-35B (STOVL), and the F-35C (CATOBAR). Despite being intended to share most of their parts to reduce costs and improve maintenance logistics, by 2017, the effective commonality was only 20%. The program received considerable criticism for cost overruns during development and for the total projected cost of the program over the lifetime of the jets.

 

By 2017, the program was expected to cost $406.5 billion over its lifetime (i.e. until 2070) for acquisition of the jets, and an additional $1.1 trillion for operations and maintenance. A number of design deficiencies were alleged, such as: carrying a small internal payload; performance inferior to the aircraft being replaced, particularly the F-16; lack of safety in relying on a single engine; and flaws such as the vulnerability of the fuel tank to fire and the propensity for transonic roll-off (wing drop). The possible obsolescence of stealth technology was also criticized.

  

Design

 

Overview

 

Although several experimental designs have been developed since the 1960s, such as the unsuccessful Rockwell XFV-12, the F-35B is to be the first operational supersonic STOVL stealth fighter. The single-engine F-35 resembles the larger twin-engined Lockheed Martin F-22 "Raptor", drawing design elements from it. The exhaust duct design was inspired by the General Dynamics Model 200, proposed for a 1972 supersonic VTOL fighter requirement for the Sea Control Ship.

 

Lockheed Martin has suggested that the F-35 could replace the USAF's F-15C/D fighters in the air-superiority role and the F-15E "Strike Eagle" in the ground-attack role. It has also stated the F-35 is intended to have close- and long-range air-to-air capability second only to that of the F-22 "Raptor", and that the F-35 has an advantage over the F-22 in basing flexibility and possesses "advanced sensors and information fusion".

 

Testifying before the House Appropriations Committee on 25 March 2009, acquisition deputy to the assistant secretary of the Air Force, Lt. Gen. Mark D. "Shack" Shackelford, stated that the F-35 is designed to be America's "premier surface-to-air missile killer, and is uniquely equipped for this mission with cutting-edge processing power, synthetic aperture radar integration techniques, and advanced target recognition".

  

Improvements

 

Ostensible improvements over past-generation fighter aircraft include:

 

Durable, low-maintenance stealth technology, using structural fiber mat instead of the high-maintenance coatings of legacy stealth platforms.

 

Integrated avionics and sensor fusion that combine information from off- and on-board sensors to increase the pilot's situational awareness and improve target identification and weapon delivery, and to relay information quickly to other command and control (C2) nodes.

 

High-speed data networking including IEEE 1394b and Fibre Channel (Fibre Channel is also used on Boeing's "Super Hornet".

 

The Autonomic Logistics Global Sustainment, Autonomic Logistics Information System (ALIS), and Computerized maintenance management system to help ensure the aircraft can remain operational with minimal maintenance manpower The Pentagon has moved to open up the competitive bidding by other companies. This was after Lockheed Martin stated that instead of costing 20% less than the F-16 per flight hour, the F-35 would actually cost 12% more. Though the ALGS is intended to reduce maintenance costs, the company disagrees with including the cost of this system in the aircraft ownership calculations. The USMC has implemented a workaround for a cyber vulnerability in the system. The ALIS system currently requires a shipping-container load of servers to run, but Lockheed is working on a more portable version to support the Marines' expeditionary operations.

 

Electro-hydrostatic actuators run by a power-by-wire flight-control system.

 

A modern and updated flight simulator, which may be used for a greater fraction of pilot training to reduce the costly flight hours of the actual aircraft.

 

Lightweight, powerful lithium-ion batteries to provide power to run the control surfaces in an emergency.

 

Structural composites in the F-35 are 35% of the airframe weight (up from 25% in the F-22). The majority of these are bismaleimide and composite epoxy materials. The F-35 will be the first mass-produced aircraft to include structural nanocomposites, namely carbon nanotube-reinforced epoxy. Experience of the F-22's problems with corrosion led to the F-35 using a gap filler that causes less galvanic corrosion to the airframe's skin, designed with fewer gaps requiring filler and implementing better drainage. The relatively short 35-foot wingspan of the A and B variants is set by the F-35B's requirement to fit inside the Navy's current amphibious assault ship parking area and elevators; the F-35C's longer wing is considered to be more fuel efficient.

  

Costs

 

A U.S. Navy study found that the F-35 will cost 30 to 40% more to maintain than current jet fighters, not accounting for inflation over the F-35's operational lifetime. A Pentagon study concluded a $1 trillion maintenance cost for the entire fleet over its lifespan, not accounting for inflation. The F-35 program office found that as of January 2014, costs for the F-35 fleet over a 53-year lifecycle was $857 billion. Costs for the fighter have been dropping and accounted for the 22 percent life cycle drop since 2010. Lockheed stated that by 2019, pricing for the fifth-generation aircraft will be less than fourth-generation fighters. An F-35A in 2019 is expected to cost $85 million per unit complete with engines and full mission systems, inflation adjusted from $75 million in December 2013.

Maker:

Born: USA

Active: USA

Medium: color dye transfer print

Size: 6.5" x 10 in

Location: USA

 

Object No. 2016.633

Shelf: A-6

 

Publication:

 

Other Collections: Library of Congress Prints & Photographs Division

 

Notes: Kodak was experimenting with the final formulation of its new Kodachrome film in the late 1930’s and decided to give some unknown number of rolls of 35mm Kodachrome film to the photographers of the FSA project to use as a pilot program. The FSA photographic project itself was historic employing some of the photographers who would become some of the most famous photographers of their generation including Walker Evans, Marion Post Wolcott, Arthur Rosenstein, Dorothea Lange, Jack Delano, Russell Lee, John Vachon and others. In an article about the photography produced by the FSA photographers Fortune Ryan and Penelope Dixon said, “The result of Stryker’s project (the FSA photography) was the radical enlargement of Americans’ capacity to to conceive redeeming images of minorities and victims of plight in general, and the elevation, at least temporarily, of photo-journalism to an aesthetic plateau equal to any previously achieved by art photography.”

 

The original transparency was lent to the Light Gallery in the 1980’s by the Library Of Congress in order to make a definitive print record of the image by the dye transfer method because of its archival and longevity characteristics and its ability to accurately reproduce the full range of the transparency. In this case the original was quite dark and had suffered color shifts which were brought to a visually acceptable balance by adjusting the color separation negs. The Light Gallery had proposed to make 250 copies each of about 60 different Kodachromes from the FSA files but the project was abandoned far short of its completion. At the best some images may have had as many as 35 copies made but others may have had as few as 10. The dye transfer printing method was also a Kodak product that was introduced in the mid 30’s to reproduce color transparencies of the Ektacolor and later the Kodachrome type. The method involved the making of enlarged color separation negatives on black and white film through a red, a green, and a blue filter which were in turn used to make relief positives on a gelatin matrix film at the size of the print which were put in colored dye baths of cyan(red filter negative), magenta(green filter negative) and yellow(blue filter negative) and finally transferred in register onto a prepared piece of photographic paper which itself had no chemistry incorporated into it(enhancing its archivality). The dyes were very stable and very bright which enabled the dye transfers to have a larger color gamut than any other color photographic printing method and longevity of up to 150 years with good handling. Kodak discontinued the manufacture of the dye transfer materials in the late 1980’s with the introduction of computerized retouching since the largest audience for the prints had been advertising agencies and publications which used the pictures to retouch and refine photos of products and portraits.

 

To view our archive organized by Collections, visit: OUR COLLECTIONS

 

For information about reproducing this image, visit: THE HISTORY OF PHOTOGRAPHY ARCHIVE

 

At the eastern end of the Garden of Champ de Mars, in front of the Ecole Militare, is the Monument to Peace, constructed in 2000. The word "peace" is written in 32 languages on 32 columns. A computerized keyboard inside the monument allows visitors to leave their personal message of peace

 

PLEASE view on black. Press L or click image.

Everything is computerized today. Even our thoughts.

Everything is at our fingertips, and human touch is, in my opinion,

very much fading.

What seems close is just the result of a cold calculation

of what I like and what my taste is, made somewhere

far away – both physically and in spirit.

But it only looks like it. Feels like it.

And it’s convenient.

But I still remember hands touching the pages and the soul

from a distance of nothing – a distance where you could feel the pulse.

Because once it was truly personal.

And today?

 

Mon choix

Tout est informatisé aujourd’hui. Même nos pensées.

Tout est au bout de nos doigts, et le contact humain, à mon avis,

s’estompe énormément.

Ce qui semble proche n’est que le résultat d’un calcul froid

de ce que j’aime et de mes goûts, fait quelque part

loin d’ici – à la fois physiquement et dans l’âme.

Mais cela ne fait que sembler. Cela donne l’impression.

Et c’est pratique.

Mais je me souviens encore des mains touchant les pages et l’âme

à une distance nulle – une distance où l’on pouvait sentir le pouls.

Car autrefois, c’était vraiment personnel.

Et aujourd’hui ?

A wrecking yard (Australian, New Zealand, and Canadian English), scrapyard (Irish and British English) or junkyard (American English) is the location of a business in dismantling where wrecked or decommissioned vehicles are brought, their usable parts are sold for use in operating vehicles, while the unusable metal parts, known as scrap metal parts, are sold to metal-recycling companies.

 

Other terms include wreck yard, wrecker's yard, salvage yard, breakers yard, dismantler and scrapheap. In the United Kingdom, car salvage yards are known as car breakers, while motorcycle salvage yards are known as bike breakers. In Australia, they are often referred to as 'Wreckers'.

 

The most common type of wreck yards are automobile wreck yards, but junkyards for motorcycles, bicycles, small airplanes and boats exist too.

 

Many salvage yards operate on a local level—when an automobile is severely damaged, has malfunctioned beyond repair, or not worth the repair, the owner may sell it to a junkyard; in some cases—as when the car has become disabled in a place where derelict cars are not allowed to be left—the car owner will pay the wrecker to haul the car away.

 

Salvage yards also buy most of the wrecked, derelict and abandoned vehicles that are sold at auction from police impound storage lots,and often buy vehicles from insurance tow yards as well.

 

The salvage yard will usually tow the vehicle from the location of its purchase to the yard, but occasionally vehicles are driven in. At the salvage yard the automobiles are typically arranged in rows, often stacked on top of one another.

 

Some yards keep inventories in their offices, as to the usable parts in each car, as well as the car's location in the yard. Many yards have computerized inventory systems. About 75% of any given vehicle can be recycled and used for other goods.

 

In recent years it is becoming increasingly common to use satellite part finder services to contact multiple salvage yards from a single source.

 

In the 20th century these were call centres that charged a premium rate for calls and compiled a facsimile that was sent to various salvage yards so they could respond directly if the part was in stock. Many of these are now Web-based with requests for parts being e-mailed instantly.

Found at the 1940s Air Terminal Museum, Houston, Texas

 

Per Wikipedia:

 

"Pan American World Airways, commonly known as Pan Am, was the principal and largest international air carrier in the United States from 1927 until its collapse on December 4, 1991. Founded in 1927 as a scheduled air mail and passenger service operating between Key West, Florida, and Havana, Cuba, the airline became a major company credited with many innovations that shaped the international airline industry, including the widespread use of jet aircraft, jumbo jets, and computerized reservation systems. It was also a founding member of the International Air Transport Association (IATA), the global airline industry association."

Quoting Smithsonian National Air and Space Museum | Dornier Do 335 A-0 Pfeil (Arrow):

 

The Do-335 was one of a small group of aircraft marking the pinnacle of international piston-engined development. It was the fastest production piston-engined fighter ever built, attaining 846 kilometers per hour (474 mph) in level flight at a time when the official world speed record was 755 kph (469 mph). Powered by two 1800-hp engines in a unique low-drag configuration and weighing 9600 kg (21,000 lb) loaded, it was an exceptional heavy fighter. This very innovative design also featured an ejection seat, for pilot safety, and a jettisoning fin.

 

The unconventional layout of the Do-335 -- one engine "pulling" in the nose and another "pushing" in the tail - was patented by Claudius Dornier in 1937. The configuration provided the power of two engines, but with reduced drag and better maneuverability. The German Aviation Ministry (RLM) was interested in the design, but initially wanted Dornier only to produce bombers. By 1942, Dornier was still continuing design work and the war situation was worsening. The Luftwaffe now needed a multi-purpose fighter, and the prototype Do-335V-1 ("V" indicating "versuchs" or "experimental") flew in fighter form in September, 1943 - six years after its conception. Orders were immediately placed for 14 prototypes, 10 A-0 preproduction aircraft, 11 production A-1 single-seaters, and 3 A-10 and A-12 two-seat trainers.

 

The aircraft was quite large for a single-seat fighter, with a cruciform tail and a tricycle landing gear. The two massive liquid-cooled Daimler-Benz DB-603 engines were used in four different versions, each displacing 44.5 liters (2670 cu in) and weighing 910 kg (2006 lb). The engine produced 1750 hp from 12 cylinders in an inverted V layout using fuel injection and an 8.3:1 compression ratio. The rear three-bladed propeller and dorsal fin were jettisoned by explosive bolts in an emergency, to allow the pilot to bail out safely using a pneumatic ejection seat. The seat, inclined 13 degrees to the rear, was ejected with a force of 20 times gravity. The ventral fin could be jettisoned for a belly landing.

 

Unlike a normal twin-engined aircraft, with wing-mounted engines, loss of an engine on the Do-335 did not cause a handling problem. Even with one engine out, speed was a respectable 621 kph (348 mph). Because of its appearance, pilots dubbed it the "Ant eater" ("Ameisenbar"), although they described its performance as exceptional, particularly in acceleration and turning radius. The Do-335 was very docile in flight and had no dangerous spin characteristics. Many Do-335 prototypes were built, as the Reich strained desperately to provide day and night fighters and fast reconnaissance aircraft to the failing war effort. One of the many RLM production plans, issued in December 1943, called for the production of 310 Do-335s by late 1945. Initial production was at the Dornier Manuel plant, but this factory was bombed heavily in March-April, 1944, and the Do-335 tooling was destroyed.

 

Ten Do-335A-0 preproduction aircraft were then produced at Dornier's Oberpfaffenhofen plant in July-October 1944, by which time the Allied bombing campaign was delaying arrivals of engines, propellers, radios, and structural subcomponents. This had a serious effect, because the Do-335 was not a simple aircraft: installation of the electronics alone took 60 hours of assembly, and the electrical parts list was 112 pages long. Production of Daimler-Benz engines, for example, was switched to factories set up in underground salt mines and gypsum mines, but high humidity caused corrosion problems and production dropped 40 percent. Although several preproduction aircraft were issued to combat conversion units some 10 months before the war ended, no Do-335s actually entered combat. Deliveries began to the 1st Experimental Squadron of the Commander-in-Chief of the Luftwaffe ( I/Versuchsverband Ob.d.L.) in late July 1944 for operational trials.

 

The first of the Do-335A-1 production version left the Dornier line at Friedrichshafen early in 1945, one of only four produced in 1945. It was armed with one 30 mm MK-103 cannon (70 rounds were carried) firing through the propeller hub and two 15 mm MG-151/15 cannon (200 rounds per gun) firing from the top of the forward engine. Even with the fighter situation as desperate as it was, these aircraft were still equipped to carry 500 kg (1100 lb) of bombs internally. Further operational testing, including use of air-to-ground guided missiles, began in Spring 1945 with Trials Unit (Erprobungskommando) 335.

 

The Do-335A-6 was to be a two-seat night fighter version with the advanced FFO FuG-217J Neptun radar having triple "trident"-like antennas (hence the name "Neptun") on the fuselage and wings, but only a prototype was completed. A total of 37 prototypes, 10 A-0s, 11 A-1s and 2 A-12 trainers were built, although nearly 85 additional aircraft were in assembly when U.S. troops overran the Friedrichshafen factory in late April, 1945. The Vienna-Swechat plant of the Ernst Heinkel AG was also scheduled to build the Do-335 beginning in February, 1945, but production never started.

 

The NASM aircraft is the second Do-335A-0, designated A-02, with construction number (werke nummer) 240102 and factory registration VG+PH. It was built at Dornier's Rechlin-Oberpfaffenhofen, Germany, plant on April 16, 1945. It was captured by Allied forces at the plant on April 22, 1945. After checkout, it was flown from a grass runway at Oberweisenfeld, near Munich, to Cherbourg, France. During this flight, the Do-335 easily outclimbed and outdistanced two escorting P-51s, beating them to Cherbourg by 45 minutes. Under the U.S. Army Air Force's "Project Sea Horse," two Do-335s were shipped to the United States aboard the Royal Navy ship HMS "Reaper" together with other captured German aircraft, for detailed evaluation. This aircraft was assigned to the U.S. Navy, which tested it at the Test and Evaluation Center, Patuxent River Naval Air Station, Maryland. The other aircraft, with registration FE-1012 (later T2-1012), went to the USAAF at Freeman Field, Indiana, where it was tested in early 1946. Its subsequent fate is unknown, and this is the only Do-335 known to exist.

 

Following Navy flight tests in 1945-48, the aircraft was donated to the Smithsonian's National Air Museum in 1961 but was stored at NAS Norfolk until 1974. It was then returned to Oberpfaffenhofen, Germany, where the Dornier company restored it to original condition in 1975. The return trip to Germany required an exemption under U.S. laws concerning the export of munitions. The Dornier craftsmen doing the restoration - many of whom had worked on the original aircraft -- were astonished to find that the explosive charges fitted to blow off the tail fin and rear propeller in an emergency were still in the aircraft and active, 30 years after their original installation! The Do-335 was put on static display at the May 1-9, 1976, Hannover Airshow, and then loaned to the Deutsches Museum in Munich, where it was on prominent display until returned to Silver Hill, MD, for storage in 1986.

 

Country of Origin:

Germany

 

Physical Description:

Twin engine, pusher / puller, fighter / bomber; grey/green, green; late World War II development.

+++ DISCLAIMER +++

Nothing you see here is real, even though the conversion or the presented background story might be based on historical facts. BEWARE!

  

Some background:

The Waffenträger (Weapon Carrier) VTS3 “Diana” was a prototype for a wheeled tank destroyer. It was developed by Thyssen-Henschel (later Rheinmetall) in Kassel, Germany, in the late Seventies, in response to a German Army requirement for a highly mobile tank destroyer with the firepower of the Leopard 1 main battle tank then in service and about to be replaced with the more capable Leopard 2 MBT, but less complex and costly. The main mission of the Diana was light to medium territorial defense, protection of infantry units and other, lighter, elements of the cavalry as well as tactical reconnaissance. Instead of heavy armor it would rather use its good power-to-weight ratio, excellent range and cross-country ability (despite the wheeled design) for defense and a computerized fire control system to accomplish this mission.

 

In order to save development cost and time, the vehicle was heavily based on the Spähpanzer Luchs (Lynx), a new German 8x8 amphibious reconnaissance armored fighting vehicle that had just entered Bundeswehr service in 1975. The all-wheel drive Luchs made was well armored against light weapons, had a full NBC protection system and was characterized by its extremely low-noise running. The eight large low-pressure tires had run-flat properties, and, at speeds up to about 50 km/h, all four axles could be steered, giving the relatively large vehicle a surprising agility and very good off-road performance. As a special feature, the vehicle was equipped with a rear-facing driver with his own driving position (normally the radio operator), so that the vehicle could be driven at full speed into both directions – a heritage from German WWII designs, and a tactical advantage when the vehicle had to quickly retreat from tactical position after having been detected. The original Luchs weighed less than 20 tons, was fully amphibious and could surmount water obstacles quickly and independently using propellers at the rear and the fold back trim vane at the front. Its armament was relatively light, though, a 20 mm Rheinmetall MK 20 Rh 202 gun in the turret that was effective against both ground and air targets.

 

The Waffenträger “Diana” used the Luchs’ hull and dynamic components as basis, and Thyssen-Henschel solved the challenge to mount a large and heavy 105 mm L7 gun with its mount on the light chassis through a minimalistic, unmanned mount and an autoloader. Avoiding a traditional manned and heavy, armored turret, a lot of weight and internal volume that had to be protected could be saved, and crew safety was indirectly improved, too. This concept had concurrently been tested in the form of the VTS1 (“Versuchsträger Scheitellafette #1) experimental tank in 1976 for the Kampfpanzer 3 development, which eventually led to the Leopard 2 MBT (which retained a traditional turret, though).

 

For the “Diana” test vehicle, Thyssen-Henschel developed a new low-profile turret with a very small frontal area. Two crew members, the commander (on the right side) and the gunner (to the left), were seated in/under the gun mount, completely inside of the vehicle’s hull. The turret was a very innovative construction for its time, fully stabilized and mounted the proven 105mm L7 rifled cannon with a smoke discharger. Its autoloader contained 8 rounds in a carousel magazine. 16 more rounds could be carried in the hull, but they had to be manually re-loaded into the magazine, which was only externally accessible. A light, co-axial 7,62mm machine gun against soft targets was available, too, as well as eight defensive smoke grenade mortars.

 

The automated L7 had a rate of fire of ten rounds per minute and could fire four types of ammunition: a kinetic energy penetrator to destroy armored vehicles; a high explosive anti-tank round to destroy thin-skinned vehicles and provide anti-personnel fragmentation; a high explosive plastic round to destroy bunkers, machine gun and sniper positions, and create openings in walls for infantry to access; and a canister shot for use against dismounted infantry in the open or for smoke charges. The rounds to be fired could be pre-selected, so that the gun was able to automatically fire a certain ammunition sequence, but manual round selection was possible at any time, too.

 

In order to take the new turret, the Luchs hull had to be modified. Early calculations had revealed that a simple replacement of the Luchs’ turret with the new L7 mount would have unfavorably shifted the vehicle’s center of gravity up- and forward, making it very nose-heavy and hard to handle in rough terrain or at high speed, and the long barrel would have markedly overhung the front end, impairing handling further. It was also clear that the additional weight and the rise of the CoG made amphibious operations impossible - a fate that met the upgraded Luchs recce tanks in the Eighties, too, after several accidents with overturned vehicles during wading and drowned crews. With this insight the decision was made to omit the vehicle’s amphibious capability, save weight and complexity, and to modify the vehicle’s layout considerably to optimize the weight distribution.

 

Taking advantage of the fact that the Luchs already had two complete driver stations at both ends, a pair of late-production hulls were set aside in 1977 and their internal layout reversed. The engine bay was now in the vehicle’s front, the secured ammunition storage was placed next to it, behind the separate driver compartment, and the combat section with the turret mechanism was located behind it. Since the VTS3s were only prototypes, only minimal adaptations were made. This meant that the driver was now located on the right side of the vehicle, while and the now-rear-facing secondary driver/radio operator station ended up on the left side – much like a RHD vehicle – but this was easily accepted in the light of cost and time savings. As a result, the gun and its long, heavy barrel were now located above the vehicle’s hull, so that the overall weight distribution was almost neutral and overall dimensions remained compact.

 

Both test vehicles were completed in early 1978 and field trials immediately started. While the overall mobility was on par with the Luchs and the Diana’s high speed and low noise profile was highly appreciated, the armament was and remained a source of constant concern. Shooting in motion from the Diana turned out to be very problematic, and even firing from a standstill was troublesome. The gun mount and the vehicle’s complex suspension were able to "hold" the recoil of the full-fledged 105-mm tank gun, which had always been famous for its rather large muzzle energy. But when fired, even in the longitudinal plane, the vehicle body fell heavily towards the stern, so that the target was frequently lost and aiming had to be resumed – effectively negating the benefit from the autoloader’s high rate of fire and exposing the vehicle to potential target retaliation. Firing to the side was even worse. Several attempts were made to mend this flaw, but neither the addition of a muzzle brake, stronger shock absorbers and even hydro-pneumatic suspension elements did not solve the problem. In addition, the high muzzle flames and the resulting significant shockwave required the infantry to stay away from the vehicle intended to support them. The Bundeswehr also criticized the too small ammunition load, as well as the fact that the autoloader magazine could not be re-filled under armor protection, so that the vehicle had to retreat to safe areas to re-arm and/or to adapt to a new mission profile. This inherent flaw not only put the crew under the hazards of enemy fire, it also negated the vehicle’s NBC protection – a serious issue and likely Cold War scenario. Another weak point was the Diana’s weight: even though the net gain of weight compared with the Luchs was less than 3 tons after the conversion, this became another serious problem that led to the Diana’s demise: during trials the Bundeswehr considered the possibility to airlift the Diana, but its weight (even that of the Luchs, BTW) was too much for the Luftwaffe’s biggest own transport aircraft, the C-160 Transall. Even aircraft from other NATO members, e.g. the common C-130 Hercules, could hardly carry the vehicle. In theory, equipment had to be removed, including the cannon and parts of its mount.

 

Since the tactical value of the vehicle was doubtful and other light anti-tank weapons in the form of the HOT anti-tank missile had reached operational status, so that very light vehicles and even small infantry groups could now effectively fight against full-fledged enemy battle tanks from a safe distance, the Diana’s development was stopped in 1988. Both VTS3 prototypes were mothballed, stored at the Bundeswehr Munster Training Area camp and are still waiting to be revamped as historic exhibits alongside other prototypes like the Kampfpanzer 70 in the German Tank Museum located there, too.

  

Specifications:

Crew: 4 (commander, driver, gunner, radio operator/second driver)

Weight: 22.6 t

Length: 7.74 m (25 ft 4 ¼ in)

Width: 2.98 m ( 9 ft 9 in)

Height: XXX

Ground clearance: 440 mm (1 ft 4 in)

Suspension: hydraulic all-wheel drive and steering

 

Armor:

Unknown, but sufficient to withstand 14.5 mm AP rounds

 

Performance:

Speed: 90 km/h (56 mph) on roads

Operational range: 720 km (445 mi)

Power/weight: 13,3 hp/ton with petrol, 17,3 hp/ton with diesel

 

Engine:

1× Daimler Benz OM 403A turbocharged 10-cylinder 4-stroke multi-fuel engine,

delivering 300 hp with petrol, 390 hp with diesel

 

Armament:

1× 105 mm L7 rifled gun with autoloader (8 rounds ready, plus 16 in reserve)

1× co-axial 7.92 mm M3 machine gun with 2.000 rounds

Two groups of four Wegmann 76 mm smoke mortars

  

The kit and its assembly:

I have been a big Luchs fan since I witnessed one in action during a public Bundeswehr demo day when I was around 10 years old: a huge, boxy and futuristic vehicle with strange proportions, gigantic wheels, water propellers, a mind-boggling mobility and all of this utterly silent. Today you’d assume that this vehicle had an electric engine – spooky! So I always had a soft spot for it, and now it was time and a neat occasion to build a what-if model around it.

 

This fictional wheeled tank prototype model was spawned by a leftover Revell 1:72 Luchs kit, which I had bought some time ago primarily for the turret, used in a fictional post-WWII SdKfz. 234 “Puma” conversion. With just the chassis left I wondered what other use or equipment it might take, and, after several weeks with the idea in the back of my mind, I stumbled at Silesian Models over an M1128 resin conversion set for the Trumpeter M1126 “Stryker” 8x8 APC model. From this set as potential donor for a conversion the prototype idea with an unmanned turret was born.

 

Originally I just planned to mount the new turret onto the OOB hull, but when playing with the parts I found the look with an overhanging gun barrel and the bigger turret placed well forward on the hull goofy and unbalanced. I was about to shelf the idea again, until I recognized that the Luchs’ hull is almost symmetrical – the upper hull half could be easily reversed on the chassis tub (at least on the kit…), and this would allow much better proportions. From this conceptual change the build went straightforward, reversing the upper hull only took some minor PSR. The resin turret was taken mostly OOB, it only needed a scratched adapter to fit into the respective hull opening. I just added a co-axial machine gun fairing, antenna bases (from the Luchs kit, since they could, due to the long gun barrel, not be attached to the hull anymore) and smoke grenade mortars (also taken from the Luchs).

 

An unnerving challenge became the Luchs kit’s suspension and drive train – it took two days to assemble the vehicle’s underside alone! While this area is very accurate and delicate, the fact that almost EVERY lever and stabilizer is a separate piece on four(!) axles made the assembly a very slow process. Just for reference: the kit comes with three and a half sprues. A full one for the wheels (each consists of three parts, and more than another one for suspension and drivetrain!

Furthermore, the many hull surface details like tools or handles – these are more than a dozen bits and pieces – are separate, very fragile and small (tiny!), too. Cutting all these wee parts out and cleaning them was a tedious affair, too, plus painting them separately.

Otherwise the model went together well, but it’s certainly not good for quick builders and those with big fingers and/or poor sight.

  

Painting and markings:

The paint scheme was a conservative choice; it is a faithful adaptation of the Bundeswehr’s NATO standard camouflage for the European theatre of operations that was introduced in the Eighties. It was adopted by many armies to confuse potential aggressors from the East, so that observers could not easily identify a vehicle and its nationality. It consists of a green base with red-brown and black blotches, in Germany it was executed with RAL tones, namely 6031 (Bronze Green), 8027 (Leather Brown) and 9021 (Tar Black). The pattern was standardized for each vehicle type and I stuck to the official Luchs pattern, trying to adapt it to the new/bigger turret. I used Revell acrylic paints, since the authentic RAL tones are readily available in this product range (namely the tones 06, 65 and 84). The big tires were painted with Revell 09 (Anthracite).

 

Next the model was treated with a highly thinned washing with black and red-brown acrylic paint, before decals were applied, taken from the OOB sheet and without unit markings, since the Diana would represent a test vehicle. After sealing them with a thin coat of clear varnish the model was furthermore treated with lightly dry-brushed Revell 45 and 75 to emphasize edges and surface details, and the separately painted hull equipment was mounted. The following step was a cloudy treatment with watercolors (from a typical school paintbox, it’s great stuff for weathering!), simulating dust residue all over the hull. After a final protective coat with matt acrylic varnish I finally added some mineral artist pigments to the lower hull areas and created mud crusts on the wheels through light wet varnish traces into which pigments were “dusted”.

  

Basically a simple project, but the complex Luchs kit with its zillion of wee bits and pieces took time and cost some nerves. However, the result looks pretty good, and the Stryker turret blends well into the overall package. Not certain how realistic the swap of the Luchs’ internal layout would have been, but I think that the turret moved to the rear makes more sense than the original forward position? After all, the model is supposed to be a prototype, so there’s certainly room for creative freedom. And in classic Bundeswehr colors, the whole thing even looks pretty convincing.

 

+++ DISCLAIMER +++

Nothing you see here is real, even though the conversion or the presented background story might be based on historical facts. BEWARE!

  

Some background:

The Waffenträger (Weapon Carrier) VTS3 “Diana” was a prototype for a wheeled tank destroyer. It was developed by Thyssen-Henschel (later Rheinmetall) in Kassel, Germany, in the late Seventies, in response to a German Army requirement for a highly mobile tank destroyer with the firepower of the Leopard 1 main battle tank then in service and about to be replaced with the more capable Leopard 2 MBT, but less complex and costly. The main mission of the Diana was light to medium territorial defense, protection of infantry units and other, lighter, elements of the cavalry as well as tactical reconnaissance. Instead of heavy armor it would rather use its good power-to-weight ratio, excellent range and cross-country ability (despite the wheeled design) for defense and a computerized fire control system to accomplish this mission.

 

In order to save development cost and time, the vehicle was heavily based on the Spähpanzer Luchs (Lynx), a new German 8x8 amphibious reconnaissance armored fighting vehicle that had just entered Bundeswehr service in 1975. The all-wheel drive Luchs made was well armored against light weapons, had a full NBC protection system and was characterized by its extremely low-noise running. The eight large low-pressure tires had run-flat properties, and, at speeds up to about 50 km/h, all four axles could be steered, giving the relatively large vehicle a surprising agility and very good off-road performance. As a special feature, the vehicle was equipped with a rear-facing driver with his own driving position (normally the radio operator), so that the vehicle could be driven at full speed into both directions – a heritage from German WWII designs, and a tactical advantage when the vehicle had to quickly retreat from tactical position after having been detected. The original Luchs weighed less than 20 tons, was fully amphibious and could surmount water obstacles quickly and independently using propellers at the rear and the fold back trim vane at the front. Its armament was relatively light, though, a 20 mm Rheinmetall MK 20 Rh 202 gun in the turret that was effective against both ground and air targets.

 

The Waffenträger “Diana” used the Luchs’ hull and dynamic components as basis, and Thyssen-Henschel solved the challenge to mount a large and heavy 105 mm L7 gun with its mount on the light chassis through a minimalistic, unmanned mount and an autoloader. Avoiding a traditional manned and heavy, armored turret, a lot of weight and internal volume that had to be protected could be saved, and crew safety was indirectly improved, too. This concept had concurrently been tested in the form of the VTS1 (“Versuchsträger Scheitellafette #1) experimental tank in 1976 for the Kampfpanzer 3 development, which eventually led to the Leopard 2 MBT (which retained a traditional turret, though).

 

For the “Diana” test vehicle, Thyssen-Henschel developed a new low-profile turret with a very small frontal area. Two crew members, the commander (on the right side) and the gunner (to the left), were seated in/under the gun mount, completely inside of the vehicle’s hull. The turret was a very innovative construction for its time, fully stabilized and mounted the proven 105mm L7 rifled cannon with a smoke discharger. Its autoloader contained 8 rounds in a carousel magazine. 16 more rounds could be carried in the hull, but they had to be manually re-loaded into the magazine, which was only externally accessible. A light, co-axial 7,62mm machine gun against soft targets was available, too, as well as eight defensive smoke grenade mortars.

 

The automated L7 had a rate of fire of ten rounds per minute and could fire four types of ammunition: a kinetic energy penetrator to destroy armored vehicles; a high explosive anti-tank round to destroy thin-skinned vehicles and provide anti-personnel fragmentation; a high explosive plastic round to destroy bunkers, machine gun and sniper positions, and create openings in walls for infantry to access; and a canister shot for use against dismounted infantry in the open or for smoke charges. The rounds to be fired could be pre-selected, so that the gun was able to automatically fire a certain ammunition sequence, but manual round selection was possible at any time, too.

 

In order to take the new turret, the Luchs hull had to be modified. Early calculations had revealed that a simple replacement of the Luchs’ turret with the new L7 mount would have unfavorably shifted the vehicle’s center of gravity up- and forward, making it very nose-heavy and hard to handle in rough terrain or at high speed, and the long barrel would have markedly overhung the front end, impairing handling further. It was also clear that the additional weight and the rise of the CoG made amphibious operations impossible - a fate that met the upgraded Luchs recce tanks in the Eighties, too, after several accidents with overturned vehicles during wading and drowned crews. With this insight the decision was made to omit the vehicle’s amphibious capability, save weight and complexity, and to modify the vehicle’s layout considerably to optimize the weight distribution.

 

Taking advantage of the fact that the Luchs already had two complete driver stations at both ends, a pair of late-production hulls were set aside in 1977 and their internal layout reversed. The engine bay was now in the vehicle’s front, the secured ammunition storage was placed next to it, behind the separate driver compartment, and the combat section with the turret mechanism was located behind it. Since the VTS3s were only prototypes, only minimal adaptations were made. This meant that the driver was now located on the right side of the vehicle, while and the now-rear-facing secondary driver/radio operator station ended up on the left side – much like a RHD vehicle – but this was easily accepted in the light of cost and time savings. As a result, the gun and its long, heavy barrel were now located above the vehicle’s hull, so that the overall weight distribution was almost neutral and overall dimensions remained compact.

 

Both test vehicles were completed in early 1978 and field trials immediately started. While the overall mobility was on par with the Luchs and the Diana’s high speed and low noise profile was highly appreciated, the armament was and remained a source of constant concern. Shooting in motion from the Diana turned out to be very problematic, and even firing from a standstill was troublesome. The gun mount and the vehicle’s complex suspension were able to "hold" the recoil of the full-fledged 105-mm tank gun, which had always been famous for its rather large muzzle energy. But when fired, even in the longitudinal plane, the vehicle body fell heavily towards the stern, so that the target was frequently lost and aiming had to be resumed – effectively negating the benefit from the autoloader’s high rate of fire and exposing the vehicle to potential target retaliation. Firing to the side was even worse. Several attempts were made to mend this flaw, but neither the addition of a muzzle brake, stronger shock absorbers and even hydro-pneumatic suspension elements did not solve the problem. In addition, the high muzzle flames and the resulting significant shockwave required the infantry to stay away from the vehicle intended to support them. The Bundeswehr also criticized the too small ammunition load, as well as the fact that the autoloader magazine could not be re-filled under armor protection, so that the vehicle had to retreat to safe areas to re-arm and/or to adapt to a new mission profile. This inherent flaw not only put the crew under the hazards of enemy fire, it also negated the vehicle’s NBC protection – a serious issue and likely Cold War scenario. Another weak point was the Diana’s weight: even though the net gain of weight compared with the Luchs was less than 3 tons after the conversion, this became another serious problem that led to the Diana’s demise: during trials the Bundeswehr considered the possibility to airlift the Diana, but its weight (even that of the Luchs, BTW) was too much for the Luftwaffe’s biggest own transport aircraft, the C-160 Transall. Even aircraft from other NATO members, e.g. the common C-130 Hercules, could hardly carry the vehicle. In theory, equipment had to be removed, including the cannon and parts of its mount.

 

Since the tactical value of the vehicle was doubtful and other light anti-tank weapons in the form of the HOT anti-tank missile had reached operational status, so that very light vehicles and even small infantry groups could now effectively fight against full-fledged enemy battle tanks from a safe distance, the Diana’s development was stopped in 1988. Both VTS3 prototypes were mothballed, stored at the Bundeswehr Munster Training Area camp and are still waiting to be revamped as historic exhibits alongside other prototypes like the Kampfpanzer 70 in the German Tank Museum located there, too.

  

Specifications:

Crew: 4 (commander, driver, gunner, radio operator/second driver)

Weight: 22.6 t

Length: 7.74 m (25 ft 4 ¼ in)

Width: 2.98 m ( 9 ft 9 in)

Height: XXX

Ground clearance: 440 mm (1 ft 4 in)

Suspension: hydraulic all-wheel drive and steering

 

Armor:

Unknown, but sufficient to withstand 14.5 mm AP rounds

 

Performance:

Speed: 90 km/h (56 mph) on roads

Operational range: 720 km (445 mi)

Power/weight: 13,3 hp/ton with petrol, 17,3 hp/ton with diesel

 

Engine:

1× Daimler Benz OM 403A turbocharged 10-cylinder 4-stroke multi-fuel engine,

delivering 300 hp with petrol, 390 hp with diesel

 

Armament:

1× 105 mm L7 rifled gun with autoloader (8 rounds ready, plus 16 in reserve)

1× co-axial 7.92 mm M3 machine gun with 2.000 rounds

Two groups of four Wegmann 76 mm smoke mortars

  

The kit and its assembly:

I have been a big Luchs fan since I witnessed one in action during a public Bundeswehr demo day when I was around 10 years old: a huge, boxy and futuristic vehicle with strange proportions, gigantic wheels, water propellers, a mind-boggling mobility and all of this utterly silent. Today you’d assume that this vehicle had an electric engine – spooky! So I always had a soft spot for it, and now it was time and a neat occasion to build a what-if model around it.

 

This fictional wheeled tank prototype model was spawned by a leftover Revell 1:72 Luchs kit, which I had bought some time ago primarily for the turret, used in a fictional post-WWII SdKfz. 234 “Puma” conversion. With just the chassis left I wondered what other use or equipment it might take, and, after several weeks with the idea in the back of my mind, I stumbled at Silesian Models over an M1128 resin conversion set for the Trumpeter M1126 “Stryker” 8x8 APC model. From this set as potential donor for a conversion the prototype idea with an unmanned turret was born.

 

Originally I just planned to mount the new turret onto the OOB hull, but when playing with the parts I found the look with an overhanging gun barrel and the bigger turret placed well forward on the hull goofy and unbalanced. I was about to shelf the idea again, until I recognized that the Luchs’ hull is almost symmetrical – the upper hull half could be easily reversed on the chassis tub (at least on the kit…), and this would allow much better proportions. From this conceptual change the build went straightforward, reversing the upper hull only took some minor PSR. The resin turret was taken mostly OOB, it only needed a scratched adapter to fit into the respective hull opening. I just added a co-axial machine gun fairing, antenna bases (from the Luchs kit, since they could, due to the long gun barrel, not be attached to the hull anymore) and smoke grenade mortars (also taken from the Luchs).

 

An unnerving challenge became the Luchs kit’s suspension and drive train – it took two days to assemble the vehicle’s underside alone! While this area is very accurate and delicate, the fact that almost EVERY lever and stabilizer is a separate piece on four(!) axles made the assembly a very slow process. Just for reference: the kit comes with three and a half sprues. A full one for the wheels (each consists of three parts, and more than another one for suspension and drivetrain!

Furthermore, the many hull surface details like tools or handles – these are more than a dozen bits and pieces – are separate, very fragile and small (tiny!), too. Cutting all these wee parts out and cleaning them was a tedious affair, too, plus painting them separately.

Otherwise the model went together well, but it’s certainly not good for quick builders and those with big fingers and/or poor sight.

  

Painting and markings:

The paint scheme was a conservative choice; it is a faithful adaptation of the Bundeswehr’s NATO standard camouflage for the European theatre of operations that was introduced in the Eighties. It was adopted by many armies to confuse potential aggressors from the East, so that observers could not easily identify a vehicle and its nationality. It consists of a green base with red-brown and black blotches, in Germany it was executed with RAL tones, namely 6031 (Bronze Green), 8027 (Leather Brown) and 9021 (Tar Black). The pattern was standardized for each vehicle type and I stuck to the official Luchs pattern, trying to adapt it to the new/bigger turret. I used Revell acrylic paints, since the authentic RAL tones are readily available in this product range (namely the tones 06, 65 and 84). The big tires were painted with Revell 09 (Anthracite).

 

Next the model was treated with a highly thinned washing with black and red-brown acrylic paint, before decals were applied, taken from the OOB sheet and without unit markings, since the Diana would represent a test vehicle. After sealing them with a thin coat of clear varnish the model was furthermore treated with lightly dry-brushed Revell 45 and 75 to emphasize edges and surface details, and the separately painted hull equipment was mounted. The following step was a cloudy treatment with watercolors (from a typical school paintbox, it’s great stuff for weathering!), simulating dust residue all over the hull. After a final protective coat with matt acrylic varnish I finally added some mineral artist pigments to the lower hull areas and created mud crusts on the wheels through light wet varnish traces into which pigments were “dusted”.

  

Basically a simple project, but the complex Luchs kit with its zillion of wee bits and pieces took time and cost some nerves. However, the result looks pretty good, and the Stryker turret blends well into the overall package. Not certain how realistic the swap of the Luchs’ internal layout would have been, but I think that the turret moved to the rear makes more sense than the original forward position? After all, the model is supposed to be a prototype, so there’s certainly room for creative freedom. And in classic Bundeswehr colors, the whole thing even looks pretty convincing.

 

Quoting Smithsonian National Air and Space Museum | Boeing B-29 Superfortress "Enola Gay":

 

Boeing's B-29 Superfortress was the most sophisticated propeller-driven bomber of World War II and the first bomber to house its crew in pressurized compartments. Although designed to fight in the European theater, the B-29 found its niche on the other side of the globe. In the Pacific, B-29s delivered a variety of aerial weapons: conventional bombs, incendiary bombs, mines, and two nuclear weapons.

 

On August 6, 1945, this Martin-built B-29-45-MO dropped the first atomic weapon used in combat on Hiroshima, Japan. Three days later, Bockscar (on display at the U.S. Air Force Museum near Dayton, Ohio) dropped a second atomic bomb on Nagasaki, Japan. Enola Gay flew as the advance weather reconnaissance aircraft that day. A third B-29, The Great Artiste, flew as an observation aircraft on both missions.

 

Transferred from the United States Air Force.

 

Manufacturer:

Boeing Aircraft Co.

Martin Co., Omaha, Nebr.

 

Date:

1945

 

Country of Origin:

United States of America

 

Dimensions:

Overall: 900 x 3020cm, 32580kg, 4300cm (29ft 6 5/16in. x 99ft 1in., 71825.9lb., 141ft 15/16in.)

 

Materials:

Polished overall aluminum finish

 

Physical Description:

Four-engine heavy bomber with semi-monoqoque fuselage and high-aspect ratio wings. Polished aluminum finish overall, standard late-World War II Army Air Forces insignia on wings and aft fuselage and serial number on vertical fin; 509th Composite Group markings painted in black; "Enola Gay" in black, block letters on lower left nose.

The body language and pose of this man look like he is just about to give this computerized ticket machine a good talking to. I don't understand the things either... I'd rather talk to a real person.

 

Please view in full size for the best effect.

The Museum of Flight, Seattle.

 

Walking through the Concorde fuselage, I was struck by the tiny windows and somewhat cramped seats. Well, with a New York to London flight time of just under 3.5 hours, Concorde didn't need to provide its passengers with the creature comforts required to endure long-haul flights on conventional airliners.

========================================================

Here's a first-hand account of a trip on Concorde by By Jeffrey Levine in The Washington Post of December 17, 1989:

 

The Concorde -- transporter of the rich and famous, supersonic sled to sophisticated shores, chariot of the demigods -- has been around now for nearly a decade and a half.

 

Air France first went supersonic in January of 1976,featuring a flight from Paris to Rio de Janiero, and by the end of this month, the Air France Concorde will have carried about 850,000 passengers. I can now say I was one of the fleet few.

 

Not long ago, I found myself sitting in an opulent Air France lounge at New York's Kennedy Airport, swigging free champagne and waiting for the boarding announcement for the Paris-bound Concorde.

 

I tried to keep from gaping at my exquisitely outfitted and supremely blase fellow travelers, but when Sean Penn slouched over to a nearby phone, I debated whipping out my trusty auto-focus. On second thought, however, I decided I'd rather take my flight inside the plane.

 

When the lounge hostess made the boarding announcement, I drained my flute of champagne and headed for destiny at warp speed. As two nattily uniformed crew members checked my ticket and showed me to my seat, I had the sudden feeling that something was terribly wrong. In a flash I realized what was amiss: The crew members were smiling and politely helping me to stow my baggage, in startling contrast to the aloof soft-drink dispensers I've encountered on regular flights lately.

 

But as I bashed my head on a luggage rack, I realized that, in terms of passenger space, the Concorde doesn't differ much from smaller aircraft. This plane was built for speed, not comfort.

 

There are two gray-leather seats on each side of the aisle, and the cabin looks like a normal passenger jet that has shrunk to three-quarter size. The central aisle makes for frequent intimate encounters with other passengers, and even the serving carts are down-sized.

 

I settled into my seat and tried to look out the window -- a task not easily done through a window that is three panes thick and smaller than a paperback book.

 

But soon we were taxiing to the runway and lining up for takeoff. (No waiting behind scores of domestic flights for this bird!) The pilot, in elegant French-accented tones, warned us that we would be turning left immediately upon takeoff, and with that, he fired up the beast.

 

The engine note slowly grew to a sharp, overpowering, yet somehow muted whine. The plane, helping itself to plenty of runway, gradually built to a thrilling speed and nosed into the air. I was expecting to have my eyeballs pressed into my head, but there was none of the brain-compressing sensation of lift that normally comes with takeoff.

 

Instead, there was a sensation of terrific forward momentum, accompanied by a light juddering as the Concorde skimmed low over the water. This plane was in no hurry to gain altitude. True to his word, the pilot carved a sweeping left turn, the craft now beginning to shudder like a rocket sled on bumpy ice.

 

Then it leveled and began to climb -- not in a steady rise but in stages -- a shaking, racketing struggle for altitude. When I finally gathered my wits about me, I took a look at the Machmeter -- a small screen on the bulkhead registering our speed in cool green liquid crystal numbers -- to see that we were already traveling at over Mach 1, the speed of sound, or about 740 miles per hour.

 

We would soon reach a cruising altitude of 57,000 feet (as opposed to about 35,000 feet for most commercial aircraft) and a speed of Mach 2.2, or about 1,600 mph.

 

Once we reached cruising altitude and I could take stock of things, three qualities of supersonic travel became apparent.

 

First, turbulence is minimal way up there. We were not buffeted even once by wind.

 

Second, Mach 2.2 is noisy; conversation required leaning and screaming.

 

Third, at supersonic speed the Concorde produces a constant vibration, as much heard as felt, rather like driving rapidly over a smoothly packed gravel road.

 

It was as if we were flying through light sandpaper. Flying at that speed also produces heat, and when I held my face to the window I could feel warmth.

 

I decided to see what the brains of this machine looked like. I got permission to go forward and peer into the cockpit, half expecting to see only a large blinking computer up there, perhaps wearing a beret.

 

But no, there were three officers in what was a remarkably unremarkable cockpit. Absent were the video-game-like screens and computerized paraphernalia present on more modern aircraft. Instead there was the bewildering profusion of dials, gauges and switches found on the aircraft of my youth.

 

Nodding and mumbling under the captain's haughty gaze, I turned and headed for my seat. By now a line had built for the bathrooms, probably because, due to space considerations, the plane had only two bathrooms for its hundred passengers.

 

As I inched my way to the end of this squirming line, I realized that even though a person may amass tremendous wealth and travel in the most sophisticated form of transportation on earth, nothing can dispel the loss of dignity that comes of waiting in line to go to the bathroom.

 

When my turn came, I discovered that the bathrooms had been designed for a retromingent.

 

The rest of the flight? Rather uneventful. The other passengers provided little entertainment -- although one gentleman did spend the entire time wearing his raincoat, with a newspaper draped over his head and face -- and there was no movie.

 

The food was good, but almost everything was pureed and formed into a soft mold, which made for easy chewing but a disturbing feeling of infantility; the wine, however, was excellent (this was, after all, Air France).

 

Sean Penn slept the whole way. The landing was more conventional than the takeoff, although as the plane slowed to near landing speed it again turned into a shaking ox-cart.

 

Best of all, and to my mind the real element that made me a Concorde convert (besides the gift-wrapped leather folders that were handed out as gifts as we approached Paris), was the fact that we debarked in Paris after 3 1/2 hours, feeling refreshed, relaxed and ready to hit the Champs Elysees instead of a hotel pillow.

 

Air France has daily Concorde flights between New York and Paris; the current round-trip fare is $5,308.

 

From January through March, Air France will offer a special fare between New York and Paris, in conjunction with American Express; if you charge a first-class ticket ($4,422) on your American Express credit card, your ticket can be upgraded to a Concorde flight.

 

British Airways also flies the Concorde between New York and Paris; in addition, it has three Concorde flights a week from Washington to Paris, with a round-trip fare of $6,398.

 

Jeffrey Levine is a freelance writer in Chicago who usually takes the bus.

 

www.washingtonpost.com/archive/lifestyle/travel/1989/12/1...

  

Boeing's B-29 Superfortress was the most sophisticated propeller-driven bomber of World War II and the first bomber to house its crew in pressurized compartments. Although designed to fight in the European theater, the B-29 found its niche on the other side of the globe. In the Pacific, B-29s delivered a variety of aerial weapons: conventional bombs, incendiary bombs, mines, and two nuclear weapons.

 

On August 6, 1945, this Martin-built B-29-45-MO dropped the first atomic weapon used in combat on Hiroshima, Japan. Three days later, Bockscar (on display at the U.S. Air Force Museum near Dayton, Ohio) dropped a second atomic bomb on Nagasaki, Japan. Enola Gay flew as the advance weather reconnaissance aircraft that day. A third B-29, The Great Artiste, flew as an observation aircraft on both missions.

   

Transferred from the United States Air Force.

     

Manufacturer:

 

Boeing Aircraft Co.

Martin Co., Omaha, Nebr.

    

Date: 1945

   

Country of Origin: United States of America

   

Dimensions:

Overall: 900 x 3020cm, 32580kg, 4300cm (29ft 6 5/16in. x 99ft 1in., 71825.9lb., 141ft 15/16in.)

   

Materials:

Polished overall aluminum finish

   

Physical Description:

Four-engine heavy bomber with semi-monoqoque fuselage and high-aspect ratio wings. Polished aluminum finish overall, standard late-World War II Army Air Forces insignia on wings and aft fuselage and serial number on vertical fin; 509th Composite Group markings painted in black; "Enola Gay" in black, block letters on lower left nose.

  

Boeing's B-29 Superfortress was the most sophisticated, propeller-driven, bomber to fly during World War II, and the first bomber to house its crew in pressurized compartments. Boeing installed very advanced armament, propulsion, and avionics systems into the Superfortress. During the war in the Pacific Theater, the B-29 delivered the first nuclear weapons used in combat. On August 6, 1945, Colonel Paul W. Tibbets, Jr., in command of the Superfortress Enola Gay, dropped a highly enriched uranium, explosion-type, "gun-fired," atomic bomb on Hiroshima, Japan. Three days later, Major Charles W. Sweeney piloted the B-29 Bockscar and dropped a highly enriched plutonium, implosion-type atomic bomb on Nagasaki, Japan. Enola Gay flew as the advance weather reconnaissance aircraft that day. On August 14, 1945, the Japanese accepted Allied terms for unconditional surrender.

 

In the late 1930s, U. S. Army Air Corps leaders recognized the need for very long-range bombers that exceeded the performance of the B-17 Flying Fortress. Several years of preliminary studies paralleled a continuous fight against those who saw limited utility in developing such an expensive and unproven aircraft but the Air Corps issued a requirement for the new bomber in February 1940. It described an airplane that could carry a maximum bomb load of 909 kg (2,000 lb) at a speed of 644 kph (400 mph) a distance of at least 8,050 km (5,000 miles). Boeing, Consolidated, Douglas, and Lockheed responded with design proposals. The Army was impressed with the Boeing design and issued a contract for two flyable prototypes in September 1940. In April 1941, the Army issued another contract for 250 aircraft plus spare parts equivalent to another 25 bombers, eight months before Pearl Harbor and nearly a year-and-a-half before the first Superfortress would fly.

 

Among the design's innovations was a long, narrow, high-aspect ratio wing equipped with large Fowler-type flaps. This wing design allowed the B-29 to fly very fast at high altitudes but maintained comfortable handling characteristics during takeoff and landing. More revolutionary was the size and sophistication of the pressurized sections of the fuselage: the flight deck forward of the wing, the gunner's compartment aft of the wing, and the tail gunner's station. For the crew, flying at extreme altitudes became much more comfortable as pressure and temperature could be regulated. To protect the Superfortress, Boeing designed a remote-controlled, defensive weapons system. Engineers placed five gun turrets on the fuselage: a turret above and behind the cockpit that housed two .50 caliber machine guns (four guns in later versions), and another turret aft near the vertical tail equipped with two machine guns; plus two more turrets beneath the fuselage, each equipped with two .50 caliber guns. One of these turrets fired from behind the nose gear and the other hung further back near the tail. Another two .50 caliber machine guns and a 20-mm cannon (in early versions of the B-29) were fitted in the tail beneath the rudder. Gunners operated these turrets by remote control--a true innovation. They aimed the guns using computerized sights, and each gunner could take control of two or more turrets to concentrate firepower on a single target.

 

Boeing also equipped the B-29 with advanced radar equipment and avionics. Depending on the type of mission, a B-29 carried the AN/APQ-13 or AN/APQ-7 Eagle radar system to aid bombing and navigation. These systems were accurate enough to permit bombing through cloud layers that completely obscured the target. The B-29B was equipped with the AN/APG-15B airborne radar gun sighting system mounted in the tail, insuring accurate defense against enemy fighters attacking at night. B-29s also routinely carried as many as twenty different types of radios and navigation devices.

 

The first XB-29 took off at Boeing Field in Seattle on September 21, 1942. By the end of the year the second aircraft was ready for flight. Fourteen service-test YB-29s followed as production began to accelerate. Building this advanced bomber required massive logistics. Boeing built new B-29 plants at Renton, Washington, and Wichita, Kansas, while Bell built a new plant at Marietta, Georgia, and Martin built one in Omaha, Nebraska. Both Curtiss-Wright and the Dodge automobile company vastly expanded their manufacturing capacity to build the bomber's powerful and complex Curtiss-Wright R-3350 turbo supercharged engines. The program required thousands of sub-contractors but with extraordinary effort, it all came together, despite major teething problems. By April 1944, the first operational B-29s of the newly formed 20th Air Force began to touch down on dusty airfields in India. By May, 130 B-29s were operational. In June, 1944, less than two years after the initial flight of the XB-29, the U. S. Army Air Forces (AAF) flew its first B-29 combat mission against targets in Bangkok, Thailand. This mission (longest of the war to date) called for 100 B-29s but only 80 reached the target area. The AAF lost no aircraft to enemy action but bombing results were mediocre. The first bombing mission against the Japanese main islands since Lt. Col. "Jimmy" Doolittle's raid against Tokyo in April 1942, occurred on June 15, again with poor results. This was also the first mission launched from airbases in China.

 

With the fall of Saipan, Tinian, and Guam in the Mariana Islands chain in August 1944, the AAF acquired airbases that lay several hundred miles closer to mainland Japan. Late in 1944, the AAF moved the XXI Bomber Command, flying B-29s, to the Marianas and the unit began bombing Japan in December. However, they employed high-altitude, precision, bombing tactics that yielded poor results. The high altitude winds were so strong that bombing computers could not compensate and the weather was so poor that rarely was visual target acquisition possible at high altitudes. In March 1945, Major General Curtis E. LeMay ordered the group to abandon these tactics and strike instead at night, from low altitude, using incendiary bombs. These firebombing raids, carried out by hundreds of B-29s, devastated much of Japan's industrial and economic infrastructure. Yet Japan fought on. Late in 1944, AAF leaders selected the Martin assembly line to produce a squadron of B-29s codenamed SILVERPLATE. Martin modified these Superfortresses by removing all gun turrets except for the tail position, removing armor plate, installing Curtiss electric propellers, and modifying the bomb bay to accommodate either the "Fat Man" or "Little Boy" versions of the atomic bomb. The AAF assigned 15 Silverplate ships to the 509th Composite Group commanded by Colonel Paul Tibbets. As the Group Commander, Tibbets had no specific aircraft assigned to him as did the mission pilots. He was entitled to fly any aircraft at any time. He named the B-29 that he flew on 6 August Enola Gay after his mother. In the early morning hours, just prior to the August 6th mission, Tibbets had a young Army Air Forces maintenance man, Private Nelson Miller, paint the name just under the pilot's window.

 

Enola Gay is a model B-29-45-MO, serial number 44-86292. The AAF accepted this aircraft on June 14, 1945, from the Martin plant at Omaha (Located at what is today Offut AFB near Bellevue), Nebraska. After the war, Army Air Forces crews flew the airplane during the Operation Crossroads atomic test program in the Pacific, although it dropped no nuclear devices during these tests, and then delivered it to Davis-Monthan Army Airfield, Arizona, for storage. Later, the U. S. Air Force flew the bomber to Park Ridge, Illinois, then transferred it to the Smithsonian Institution on July 4, 1949. Although in Smithsonian custody, the aircraft remained stored at Pyote Air Force Base, Texas, between January 1952 and December 1953. The airplane's last flight ended on December 2 when the Enola Gay touched down at Andrews Air Force Base, Maryland. The bomber remained at Andrews in outdoor storage until August 1960. By then, concerned about the bomber deteriorating outdoors, the Smithsonian sent collections staff to disassemble the Superfortress and move it indoors to the Paul E. Garber Facility in Suitland, Maryland.

 

The staff at Garber began working to preserve and restore Enola Gay in December 1984. This was the largest restoration project ever undertaken at the National Air and Space Museum and the specialists anticipated the work would require from seven to nine years to complete. The project actually lasted nearly two decades and, when completed, had taken approximately 300,000 work-hours to complete. The B-29 is now displayed at the National Air and Space Museum, Steven F. Udvar-Hazy Center.

 

Notre-Dame de Paris ( French for "Our Lady of Paris"), also known as Notre-Dame Cathedral or simply Notre-Dame, is a historic Catholic cathedral on the eastern half of the Île de la Cité in the fourth arrondissement of Paris, France. The cathedral is widely considered to be one of the finest examples of French Gothic architecture, and it is among the largest and most well-known church buildings in the world. The naturalism of its sculptures and stained glass are in contrast with earlier Romanesque architecture.

 

As the cathedral of the Archdiocese of Paris, Notre-Dame is the parish that contains the cathedra, or official chair, of the archbishop of Paris, currently Cardinal André Vingt-Trois. The cathedral treasury is notable for its reliquary which houses some of Catholicism's most important first-class relics including the purported Crown of Thorns, a fragment of the True Cross, and one of the Holy Nails.

 

In the 1790s, Notre-Dame suffered desecration during the radical phase of the French Revolution when much of its religious imagery was damaged or destroyed. An extensive restoration supervised by Eugène Viollet-le-Duc began in 1845. A project of further restoration and maintenance began in 1991.

 

Architecture

Notre-Dame de Paris was among the first buildings in the world to use the flying buttress (arched exterior supports). The building was not originally designed to include the flying buttresses around the choir and nave but after the construction began, the thinner walls (popularized in the Gothic style) grew ever higher and stress fractures began to occur as the walls pushed outward. In response, the cathedral's architects built supports around the outside walls, and later additions continued the pattern.

 

Many small individually crafted statues were placed around the outside to serve as column supports and water spouts. Among these are the famous gargoyles, designed for water run-off, and chimeras. The statues were originally colored as was most of the exterior. The paint has worn off, but the gray stone was once covered with vivid colors. The cathedral was essentially complete by 1345. The cathedral has a narrow climb of 387 steps at the top of several spiral staircases; along the climb it is possible to view its most famous bell and its gargoyles in close quarters, as well as having a spectacular view across Paris when reaching the top. The design of St. Peter's Anglican Cathedral in Adelaide, Australia was inspired by Notre-Dame de Paris.

 

Construction history

 

In 1160, because the church in Paris had become the "Parisian church of the kings of Europe", Bishop Maurice de Sully deemed the previous Paris cathedral, Saint-Étienne (St Stephen's), which had been founded in the 4th century, unworthy of its lofty role, and had it demolished shortly after he assumed the title of Bishop of Paris. As with most foundation myths, this account needs to be taken with a grain of salt; archeological excavations in the 20th century suggested that the Merovingian Cathedral replaced by Sully was itself a massive structure, with a five-aisled nave and a facade some 36m across. It seems likely therefore that the faults with the previous structure were exaggerated by the Bishop to help justify the rebuilding in a newer style. According to legend, Sully had a vision of a glorious new cathedral for Paris, and sketched it on the ground outside the original church.

 

To begin the construction, the bishop had several houses demolished and had a new road built in order to transport materials for the rest of the cathedral. Construction began in 1163 during the reign of Louis VII, and opinion differs as to whether Sully or Pope Alexander III laid the foundation stone of the cathedral. However, both were at the ceremony in question. Bishop de Sully went on to devote most of his life and wealth to the cathedral's construction. Construction of the choir took from 1163 until around 1177 and the new High Altar was consecrated in 1182 (it was normal practice for the eastern end of a new church to be completed first, so that a temporary wall could be erected at the west of the choir, allowing the chapter to use it without interruption while the rest of the building slowly took shape). After Bishop Maurice de Sully's death in 1196, his successor, Eudes de Sully (no relation) oversaw the completion of the transepts and pressed ahead with the nave, which was nearing completion at the time of his own death in 1208. By this stage, the western facade had also been laid out, though it was not completed until around the mid-1240s. Over the construction period, numerous architects worked on the site, as is evidenced by the differing styles at different heights of the west front and towers. Between 1210 and 1220, the fourth architect oversaw the construction of the level with the rose window and the great halls beneath the towers.

 

The most significant change in design came in the mid 13th century, when the transepts were remodeled in the latest Rayonnant style; in the late 1240s Jean de Chelles added a gabled portal to the north transept topped off by a spectacular rose window. Shortly afterwards (from 1258) Pierre de Montreuil executed a similar scheme on the southern transept. Both these transept portals were richly embellished with sculpture; the south portal features scenes from the lives of St Stephen and of various local saints, while the north portal featured the infancy of Christ and the story of Theophilus in the tympanum, with a highly influential statue of the Virgin and Child in the trumeau.

 

Crypt

The Archaeological Crypt of the Paris Notre-Dame was created in 1965 to protect a range of historical ruins, discovered during construction work and spanning from the earliest settlement in Paris to the modern day. The crypts are managed by the Musée Carnavalet and contain a large exhibit, combining detailed models of the architecture of different time periods, and how they can be viewed within the ruins. The main feature still visible is the under-floor heating installed during the Roman occupation.

 

Organ and organists

Though several organs were installed in the cathedral over time, the earliest ones were inadequate for the building.[citation needed] The first more noted organ[citation needed] was finished in the 18th century by the noted builder François-Henri Clicquot. Some of Clicquot's original pipework in the pedal division continues to sound from the organ today. The organ was almost completely rebuilt and expanded in the 19th century by Aristide Cavaillé-Coll.

 

The position of titular organist ("head" or "chief" organist) at Notre-Dame is considered one of the most prestigious organist posts in France, along with the post of titular organist of Saint Sulpice in Paris, Cavaillé-Coll's largest instrument.

 

The organ has 7,374 pipes, with ca 900 classified as historical. It has 110 real stops, five 56-key manuals and a 32-key pedalboard. In December 1992, a two-year restoration of the organ was completed that fully computerized the organ under three LANs (Local Area Networks). The restoration also included a number of additions, notably two further horizontal reed stops en chamade in the Cavaille-Coll style. The Notre-Dame organ is therefore unique in France in having five fully independent reed stops en chamade.

 

Among the best-known organists at Notre-Dame de Paris was Louis Vierne, who held this position from 1900 to 1937. Under his tenure, the Cavaillé-Coll organ was modified in its tonal character, notably in 1902 and 1932. Léonce de Saint-Martin held the post between 1932 and 1954. Pierre Cochereau initiated further alterations (many of which were already planned by Louis Vierne), including the electrification of the action between 1959 and 1963. The original Cavaillé-Coll console, (which is now located near the organ loft), was replaced by a new console in Anglo-American style and the addition of further stops between 1965 and 1972, notably in the pedal division, the recomposition of the mixture stops, a 32' plenum in the Neo-Baroque style on the Solo manual, and finally the adding of three horizontal reed stops "en chamade" in the Iberian style.

 

After Cochereau's sudden death in 1984, four new titular organists were appointed at Notre-Dame in 1985: Jean-Pierre Leguay Olivier Latry, Yves Devernay (who died in 1990), and Philippe Lefebvre This was reminiscent of the 18th-century practice of the cathedral having four titular organists, each one playing for three months of the year.

 

Bells

The cathedral has 10 bells. The largest, Emmanuel, original to 1681, is located in the south tower and weighs just over 13 tons and is tolled to mark the hours of the day and for various occasions and services. This bell is always rung first, at least 5 seconds before the rest. Until recently, there were four additional 19th-century bells on wheels in the north tower, which were swing chimed. These bells were meant to replace nine which were removed from the cathedral during the Revolution and were rung for various services and festivals. The bells were once rung by hand before electric motors allowed them to be rung without manual labor. When it was discovered that the size of the bells could cause the entire building to vibrate, threatening its structural integrity, they were taken out of use. The bells also had external hammers for tune playing from a small clavier.

 

On the night of 24 August 1944 as the Île de la Cité was taken by an advance column of French and Allied armoured troops and elements of the Resistance, it was the tolling of the Emmanuel that announced to the city that its liberation was under way.

 

In early 2012, as part of a €2 million project, the four old bells in the north tower were deemed unsatisfactory and removed. The plan originally was to melt them down and recast new bells from the material. However, a legal challenge resulted in the bells being saved in extremis at the foundry.[11] As of early 2013, they are still merely set aside until their fate is decided. A set of 8 new bells was cast by the same foundry in Normandy that had cast the four in 1856. At the same time, a much larger bell called Marie was cast in the Netherlands—it now hangs with Emmanuel in the south tower. The 9 new bells, which were delivered to the cathedral at the same time (31 January 2013),[12] are designed to replicate.

 

+++ DISCLAIMER +++

Nothing you see here is real, even though the model, the conversion or the presented background story might be based historical facts. BEWARE!

  

Some background:

The T-54 and T-55 tanks were a series of Soviet main battle tanks introduced in the years following the Second World War. The first T-54 prototype was completed at Nizhny Tagil by the end of 1945. Initial production ramp up settled for 1947 at Nizhny Tagil, and 1948 for Kharkiv were halted and curtailed as many problems were uncovered; the T-34-85 still accounted for 88 percent of production through the 1950s.The T-54 eventually became the main tank for armored units of the Soviet Army, armies of the Warsaw Pact countries, and many others. T-54s and T-55s have been involved in many of the world's armed conflicts since the later part of the 20th century.

 

The T-54/55 series eventually became the most-produced tank in history. Estimated production numbers for the series range from 86,000 to 100,000. They were replaced by the T-62, T-64, T-72, T-80 and T-90 tanks in the Soviet and Russian armies but remain in use by up to 50 other armies worldwide, some having received sophisticated retrofitting.

The T-54/55 tanks were mechanically simple and robust, very simple to operate compared to Western tanks, and did not require a high level of training or education in their crew members. The T-54/55 was a relatively small main battle tank, presenting a smaller target for its opponents to hit. The tanks had good mobility thanks to their relatively light weight (which permitted easy transport by rail or flatbed truck and allowed crossing of lighter bridges), wide tracks (which gave lower ground pressure and hence good mobility on soft ground), a good cold-weather start-up system and a snorkel that allowed river crossings.

 

By the standards of the 1950s, the T-54 was an excellent tank combining lethal firepower, excellent armor protection and good reliability while remaining a significantly smaller and lighter tank than its NATO contemporaries—the US M48 Patton tank and the British Centurion tank. The 100 mm D-10T tank gun of the T-54 and the T-55 was also more powerful than its Western counterparts at that time (the M48 Patton initially carried a 90 mm tank gun and the Centurion Mk. 3 carried the 20-pounder (84 mm) tank gun). This advantage lasted until the T-54 began to be countered by newer Western developments like the M60 main battle tank and upgraded Centurions and M48 Pattons using the 105 mm rifled Royal Ordnance L7 or M68 gun. Due to the lack of a sub-caliber round for the 100 mm gun, and the tank's simple fire-control system, the T-54/55 was forced to rely on HEAT shaped-charge ammunition to engage tanks at long range well into the 1960s, despite the relative inaccuracy of this ammunition at long ranges. The Soviets considered this acceptable for a potential European conflict, until the development of composite armor began reducing the effectiveness of HEAT warheads and sabot rounds were developed for the D-10T gun.

 

T-54/55 tanks also had their drawbacks. Small size was achieved at the expense of interior space and ergonomics, which caused practical difficulties, as it constrained the physical movements of the crew and slowed operation of controls and equipment. This was a common trait of most Soviet tanks and hence height limits were set for certain tank crew positions in the Soviet Army.

The low turret profile of the tanks prevented them from depressing their main guns by more than 5° since the breech would strike the ceiling when fired, which limited the ability to cover terrain by fire from a hull-down position on a reverse slope – a tactical flaw that became apparent (and costly) during the Arab-Israeli the Six-Day War. As in most tanks of that generation, the internal ammunition supply was not shielded, increasing the risk that any enemy penetration of the fighting compartment could cause a catastrophic secondary explosion. The original T-54 lacked NBC protection, a revolving turret floor (which complicated the crew's operations), and early models lacked gun stabilization. All of these problems were corrected in the otherwise largely identical T-55 tank.

Together, the T-54/55 tanks have been manufactured in the tens of thousands, and many still remain in reserve, or even in front-line use among lower-technology fighting forces. Abundance and age together make these tanks cheap and easy to purchase. While the T-54/55 is not a match for a modern main battle tank, armor and ammunition upgrades could dramatically improve the old vehicle's performance to the point that it cannot be dismissed on the battlefield.

 

During the Cold War, Soviet tanks never directly faced their NATO adversaries in combat in Europe, but it became involved in many other local conflicts. For instance, the Israeli army fought against it during the Six-Day War in 1967, and many Egyptian and Syrian T-54/55s were captured. Their numbers were so great that they were repaired, modernized and even put into IDF service or exported - around 200 T-54s, T-55s and PT-76s fell into Israeli hands at that time. T-54s and T-55s were modernized to Tiran 4 or 5 standard prior to the Yom Kippur War, some outfitted with a NATO-compatible Sharir (Royal Ordnance L7) 105 mm gun and other Western equipment and weapons.

 

During the Yom Kippur War in 1973, Israel captured additional T-54s and T-55s, and these new vehicles led to the Ti-51 MBT (also known as “Tiran 51”)and some minor variants. This time the modifications were more thorough and included fitting an American Detroit Diesel engine, new semi-automatic hydromechanical transmission equipped with a torque converter and new air cleaners. Blazer explosive reactive armor was added to the hull and turret, a Cadillac-Gage-Textron gun stabilization system was integrated as well as an EL-OP Matador computerized fire control system. Further changes included a new low-profile commander's cupola, IR detectors, Image-intensifier night vision equipment for the commander, gunner and driver, Spectronix fire detection and suppression system, new turret basket, extensive external stowage, modernized driver's station including replacement of tillers by a steering wheel, new final drives, new all-internal fuel system and improved suspension. Basically, the T-54/55 hull was filled with new equipment, creating an almost new and different MBT! Some of these tanks were also outfitted with a detachable dozer blade and designated Ti-51Sh.

 

A small series of the captured Yom Kippur War tanks was furthermore re-built as so-called Ti-52s during 1974 and 1975. This program was focused on recycling T-54 and T-55 hulls that had damaged turrets or main weapons. The upgrade centered around an American 90 mm M41 cannon with a T-shaped blast deflector as new main armament, a weapon that was available in abundance after the IDF’s gun uprating of its M48 Patton tanks to the bigger L7 gun. For the Ti-52 a new, welded turret was devised, tailored to the M41 gun and its M87 mount. It was longer but narrower than the original T-54/55 turtle shell turret, but kept its low profile, and it featured prominent storage boxes at the sides and at the back that made it look outwardly bigger than it actually was. The turret had a 360° manual and electric-hydraulic traverse, (24°/sec) and the gun could be depressed to -9° and elevated to +19°. 60 rounds were carried (Fifteen in the turret, the rest in the hull). Beyond standard HE and AP ammunition types, a special HVAP round with a muzzle velocity of 3,750 ft/s (1,140 m/s) was available, too, with a maximum penetration of 15 in (380 mm) of vertical armor at 30 ft and still 9½ in (241 mm) at 2.000 yards. This was complemented by a coaxial heavy Browning .50 cal (12.7 mm) machine gun with 500 rounds (plus 500 more in reserve), a weapon that has proven to be useful and effective in asymmetric warfare. An additional .30 AA machine gun on a swivel mount and with 5.000 rounds in store was placed on the turret roof, next to the commander cupola.

The main automotive upgrade was the replacement of the original V12-W-55 engine with 560 hp with the proven American Detroit Diesel 8V-71T developing 609 hp that had already been used for other Tiran conversions. With a slightly better power/weaight ration than the original T-55 (the lighter turret and engine saved around 2 tons), performanca and handling of the Ti-52 were improved.

Other modifications included a laser rangefinder placed over the barrel, thermal/night sights for the gunner and commander, a computerized FCS, new radio equipment, complete NBC protection lining and anti-RPG rubber side skirts that also suppressed dust clouds while on the move as well as German-made smoke dischargers.

 

These upgraded vehicles entered service in 1975. With the conversion and different systems came a new role: The Ti-52s went from being an MBT to a tank destroyer and scout/reconnaissance vehicle. The Ti-52 was an ‘ambush predator’ and would use its small size, low profile and good maneuverability to outflank the enemy, engage, and then withdraw along pre-arranged lanes of engagement. The Ti-52 was unofficially nicknamed “עקרב/Ak'rav” (Scorpion) and became a successful conversion, but by the end of the Cold War in the early 1990s, the tank (just like the other Israeli Tiran versions as well as the original T-54/55 family) had become obsolete. Its gun simply did not have the penetrative power to combat modern armored fighting vehicles. Nevertheless, the tank served the Israeli Army well for 15 years, and it was used in combat during the 1982 Lebanon War, where it proved to be highly effective if its tactical strengths of speed and low profile could be exploited. In direct open-field confrontation it turned out to be vulnerable, esp. to dedicated anti-tank weapons of the time (AT-3 Sagger and RPG-7).

 

All Tirans of various versions were withdrawn from active IDF service at the end of the 1980s. Some were sold and some were converted into Achzarit APCs. However, some Tirans are still in possession of the Israeli Army, possibly in reserve or in storage. The Israeli Army had 488 Tirans in 1990, 300 in 1995, 200 in 2000, 2001 and 2002 and still 261 in 2006 and 2008.

  

Specifications:

Crew: Four (commander, gunner, loader, driver)

Weight: 34 tonnes (37.5 ST)

Length: 8,42 m (27 ft 7 in) with gun forward

6,37 m (20ft 10 1/2 in) hull only

Width: 3.53 m (11 ft 6 3/4 in) with side skirts

3.37 m (11 ft 1 in) hull only

Height: 2.73 m (9 ft)

Ground clearance: 0.425 m (16.73 in)

Suspension: Torsion bar

Fuel capacity: 580 l internal, plus 320 l external and 400 l in two jettisonable rear drums

 

Armor:

16 – 120 mm (0.63 – 4.72 in)

 

Performance:

Maximum road speed: 54 km/h (33.5 mph)

Off-road speed: 38 km/h (24 mph)

Operational range: 500 km on road

Up to 715 km with two 200-liter auxiliary fuel tanks

Power/weight: 17.9 hp (12.9 kW)/tonne

 

Engine:

1× American Detroit Diesel 8V-71T with 609 hp (438 kW)

 

Transmission:

Mechanical [synchromesh], 5 forward, 1 reverse gears

 

Armament:

1× 90mm M41/T139 gun with 60 rounds

1x coaxial .50 cal (12.7 mm) machine gun with a total of 1.000 rounds

1x .30 AA machine gun on a swivel mount with a total of 5.000 rounds

2x4 smoke grenade launchers

 

The kit and its assembly:

This is actually the second submissiion to the "Captured!" group build at whatifmodellers.com in November 2020, but since my first project stalled (waiting for parts that I ordered while building) I started this second tank and it made very quick progress.

 

Thsi what-if model has a concrete background: Israel captured during the Six Day War and the Yom Kippur conflict a lot of various Arabian tanks, including T-54/55s, PT-76s and T-62. Their numbers were so huge that many were converted on a serial basis and adopted into Israeli service or exported. So, this one became one of those modified T-55s with a new turret/gun, ERA and anti-RPG rubber side skirts. Inspiration was a little the Austrian "Kürassier" tank hunter, and the idea that many surplus 90 mm guns from upgraded M48 Patton tanks must have been available. So, why not combine everything into a dedicated IDF tank hunter?

 

The basis is a Trumpeter kit which went together well, just some PSR was necessary around the rear. I omitted the extra fuel drums (Israel is a rather small country...) and added some ERA plates to the front glacis plate. The biggest change is a different turret and mudguards, which come from an upgraded, late Danish M41 Walker Bulldog conversion set from S&S Models. It consists of a resin turret and many white metal parts, including the gun and the mantlet, the side skirts and some other stuff. The set is actually intended for a diecast M41 (Amercom/Altaya, Hobbymaster or Warmaster) as basis, but the parts were easy to integrate into the T-55 hull. The turret ring is a little smaller, so that a few spacers hold the new turret in place. The turret itself was taken OOB (including the smoke grenade dischargers), I just added the light machine gun and the swivel mount on the roof. IIRC, they are leftover pieces from an Italeri Merkava (very suitable!). The white metal mantlet and the resin turret were "bridged" with a woven dust cover, made from tissue paper dipped in white glue.

 

Themudguards are white metal pieces and needed some tailoring to fit at the front. They are actually a little too short for the T-55 hull, but taken "as is" they offered a nice opening for the drive sprocket wheels at the rear, and I settled for this simple solution.

  

Painting and markings:

Painting was done with paints from the rattle can - I chose a "Sinai Grey" livery for operations in the Southern regions (in the North, IDF tanks tend to be painted olive drab). After the base coat in two very similar shades of dark sand /RAL 7008 and 8000) the model received a black ink washing and dry-brushing with khaki drill (Humbrol 72) and later some light grey (Revell 75); the camouflage nets in the storage baskets were painted in olive drab (Humbrol 155) for some contrast.

The markings/decals come from a generic IDF markings set from Peddinghaus Decals. The Israeli marking system entered service after 1960 and it is still used today by the IDF, even if the meanings of some symbols are still unknown or unclear.

The white stripes on the cannon barrel identify which battalion the tank belongs to. If the tank belongs to the 1st Battalion, it only has one stripe on the barrel, if it is the 2nd Battalion, it has two stripes, and so on.

The company the tank belongs to is determined by a white Chevron, a white ‘V’ shaped symbol painted on the sides of the vehicle sometimes with a black outline. If the M-50 belonged to the 1st Company, the Chevron was pointing downwards, if the tank belonged to the 2nd Company, the ‘V’ was pointing forward. If the Chevron was pointed upwards, the vehicle belonged to the 3rd Company, and, if it pointed backward it belonged to the 4th Company.

The company identification markings have different sizes according to the space a tank has on its sides. The M48 Patton had these symbols painted on the turret and were quite big, while the Centurion had them painted on the side skirts. The Shermans had little space on the sides, and therefore, the company identification markings were painted on the side boxes, or in some cases, on the sides of the gun mantlet.

The platoon identification markings are written on the turrets and are divided in two: a number from 1 to 4 and one of the first four letters of the Hebrew alphabet: א (Aleph), ב (bet), ג (gimel) and ד (dalet ). The Arabic number, from 1 to 4, indicates the platoon to which a tank belongs to and the letter, the tank number inside each platoon. Tank number 1 of the 1st Platoon would have painted on the turret the symbol ‘1א’, tank number 2 of 3rd Platoon would have painted on the turret the symbol ‘3ב’, and so on. The platoon’s command tank only has the number without the letter, or in rare cases, the platoon commander has א, i.e. the first tank of the platoon.

 

Once painting and decals were done, the kit received an overall coat with matt acrylic varnish and final assembly started - namely the attempt to mount the wheels and tracks inside/thorugh the mudguards. Fiddly affair, but it worked better than expected, and as a final step I dusted the model with sand-grey mineral artist pigments.

+++ DISCLAIMER +++

Nothing you see here is real, even though the model, the conversion or the presented background story might be based on historical facts. BEWARE!

  

Some background:

After the country's independence from the United Kingdom, after its departure from the European Union in 2017, the young Republic of Scotland Air Corps (locally known as Poblachd na h-Alba Adhair an Airm) started a major procurement program to take over most basic duties the Royal Air Force formerly had taken over in Northern Britain. This procurement was preceded by a White Paper published by the Scottish National Party (SNP) in 2013, which had stated that an independent Scotland would have an air force equipped with up to 16 air defense aircraft, six tactical transports, utility rotorcraft and maritime patrol aircraft, and be capable of “contributing excellent conventional capabilities” to NATO. According to the document, “Key elements of air forces in place at independence, equipped initially from a negotiated share of current UK assets, will secure core tasks, principally the ability to police Scotland’s airspace, within NATO.” An in-country air command and control capability would be established within five years of a decision in favor of independence, it continues, with staff also to be “embedded within NATO structures”.

 

Outlining its ambition to establish an air force with an eventual 2,000 uniformed personnel and 300 reservists, the SNP stated the organization would initially be equipped with “a minimum of 12 interceptors in the Eurofighter/Typhoon class, based at Lossiemouth, a tactical air transport squadron, including around six Lockheed Martin C-130J Hercules, and a helicopter squadron”. The latter would not only have to take over transport duties for the army, there was also a dire need to quickly replace the former Royal Air Force’s Search and Rescue (SAR) capabilities and duties in the North with domestic resources, after this role was handed over to civilian contractor Bristow Helicopters and the RAF’s SAR units had been disbanded.

 

This led to the procurement of six AS365 Dauphin helicopters as an initial measure to keep up basic SAR capabilities, with the prospects of procuring more to become independent from the Bristow Helicopters contract. These aircraft were similar to the Eurocopter SA 366 MH-65 “Dolphin” for the United States Coast Guard but differed in many ways from them and also from any other navalized SA365 variant.

For the RoScAC’s SAR squadron, the SA 365 was taken as a starting point, but the helicopter was heavily modified and locally re-christened “Leumadair” (= Dolphin).

 

The most obvious new feature of the unique Scottish rescue variant was a fixed landing gear with the main wheels on short “stub wings” for a wider stance, stabilizing the helicopter during shipboard landings and in case of an emergency water landing - the helicopter was not able to perform water landings, even though inflatable emergency landing floats were typically fitted. Another obvious difference to other military Dauphin versions was the thimble radome on the nose for an RDR-1600 search and weather radar which is capable of detecting small targets at sea as far as 25 nautical miles away. This layout was chosen to provide the pilots with a better field of view directrly ahead of the helicopter. Additionally, an electro-optical sensor turret with an integrated FLIR sensor was mounted in a fully rotatable turret under the nose, giving the helicopter full all-weather capabilities. Less obvious were a digital glass cockpit and a computerized flight management system, which integrated state-of-the-art communications and navigation equipment. This system provided automatic flight control, and at the pilot's direction, the system would bring the aircraft to a stable hover 50 feet (15 m) above a selected object, an important safety feature in darkness or inclement weather. Selected search patterns could be flown automatically, freeing the pilot and copilot to concentrate on sighting & searching the object.

To improve performance and safety margin, more powerful Turbomeca Arriel 2C2-CG engines were used. Seventy-five percent of the structure—including rotor head, rotor blades and fuselage—consisted of corrosion-resistant composite materials. The rotor blades themselves were new, too, with BERP “paddles”at their tips, a new aerofoil and increased blade twist for increased lifting-capability and maximum speed, to compensate for the fixed landing gear and other external equipment that increased drag. To prevent leading edge erosion the blade used a rubber-based tape rather than the polyurethane used on earlier helicopters.

 

The “Leumadair HR.1”, so its official designation, became operational in mid-2019. Despite being owned by the government, the helicopters received civil registrations (SC-LEA - -LEF) and were dispersed along the Scottish coastline. They normally carried a crew of four: Pilot, Copilot, Flight Mechanic and Rescue Swimmer, even though regular flight patrols were only excuted with a crew of three. The Leumadair HR.1 was used by the RoScAC primarily for search and rescue missions, but also for homeland security patrols, cargo, drug interdiction, ice breaking, and pollution control. While the helicopters operated unarmed, they could be outfitted with manually operated light or medium machine guns in their doors.

However, the small fleet of only six helicopters was far from being enough to cover the Scottish coast and the many islands up north, so that the government prolonged the contract with Bristow Helicopters in late 2019 for two more years, and the procurement of further Leumadair HR.1 helicopters was decided in early 2020. Twelve more helicopters were ordered en suite and were expected to arrive in late 2021.

  

General characteristics:

Crew: 2 pilots and 2 crew

Length: 12,06 m (39 ft 2 1/2 in)

Height: 4 m (13 ft 1 in)

Main rotor diameter: 12,10 m (39 ft 7 1/2 in)

Main rotor area: 38.54 m² (414.8 sq ft)

Empty weight: 3,128 kg (6,896 lb)

Max takeoff weight: 4,300 kg (9,480 lb)

 

Powerplant:

2× Turbomeca Arriel 2C2-CG turboshaft engines, 636 kW (853 hp) each

 

Performance:

Maximum speed: 330 km/h (210 mph, 180 kn)

Cruise speed: 240 km/h (150 mph, 130 kn)

Range: 658 km (409 mi, 355 nmi)

Service ceiling: 5,486 m (17,999 ft)

 

Armament:

None installed, but provisions for a 7.62 mm M240 machine gun or a Barrett M107 0.50 in (12.7

mm) caliber precision rifle in each side door

  

The kit and its assembly:

Another chapter in my fictional alternative reality in which Scotland became an independent Republic and separated from the UK in 2017. Beyond basic aircraft for the RoScAC’s aerial defense duties I felt that maritime rescue would be another vital task for the nascent air force – and the situation that Great Britain had outsourced the SAR job to a private company called for a new solution for the independent Scotland. This led to the consideration of a relatively cheap maritime helicopter, and my choice fell on the SA365 ‘Daupin’, which has been adapted to such duties in various variants.

 

As a starting point there’s the Matchbox SA365 kit from 1983, which is a typical offer from the company: a solid kit, with mixed weak spots and nice details (e. g. the cockpit with a decent dashboard and steering columns/pedals for the crew). Revell has re-boxed this kit in 2002 as an USCG HH-65A ‘Dolphin’, but it’s technically only a painting option and the kit lacks any optional parts to actually build this type of helicopter in an authentic fashion - there are some subtle differences, and creating a convincing HH-65 from it would take a LOT of effort. Actually, it's a real scam from Revell to market the Matchbox Dauphin as a HH-65!

 

However, it was my starting basis, and for a modernized/navalized/military version of the SA365 I made some changes. For instance, I gave the helicopter a fixed landing gear, with main wheels stub wings taken from a Pavla resin upgrade/conversion set for a Lynx HAS.2, which also comes with better wheels than the Matchbox kit. The Dauphin’s landing gear wells were filled with 2C putty and in the same process took the stub wings. The front landing gear well was filled with putty, too, and a adapter to hold the front twin wheel strut was embedded. Lots of lead were hidden under the cockpit floor to ensure that this model would not becaome a tail sitter.

A thimble radome was integrated into the nose with some PSR – I opted for this layout because the fixed landing gear would block 360° radar coverage under the fuselage, and there’s not too much ground clearance or space above then cabin for a radome. Putting it on top of the rotor would have been the only other option, but I found this rather awkward. As a side benefit, the new nose changes the helicopter’s silhouette well and adds to a purposeful look.

 

The rotor blades were replaced with resin BERP blades, taken from another Pavla Lynx conversion set (for the Hobby Boss kit). Because their attachment points were very different from the Matchbox Dauphin rotor’s construction, I had to improvise a little. A rather subtle change, but the result looks very plausible and works well. Other external extras are two inflatable floating devices along the lower fuselage from a Mistercraft ASW AB 212 (UH-1) kit, the winch at port side was scratched with a piece from the aforementioned BK 117 and styrene bits. Some blade antennae were added and a sensor turret was scratched and placed in front of the front wheels. Additional air scoops for the gearbox were added, too. Inside, I added two (Matchbox) pilot figures to the cockpit, plus a third seat for a medic/observer, a storage/equipment box and a stretcher from a Revell BK 117 rescue helicopter kit. This kit also donated some small details like the rear-view mirror for the pilot and the wire-cutters - not a typical detail for a helicopter operating over the open sea, but you never know...

 

The only other adition is a technical one: I integrated a vertical styrene pipe behind the cabin as a display holder adapter for the traditional hoto shooting's in-flight scenes.

  

Painting and markings:

It took some time to settle upon a design. I wanted something bright – initially I thought about Scottish colors (white and blue), but that was not garish enough, even with some dayglo additions. The typical all-yellow RAF SAR livery was also ruled out. In the end I decided to apply a more or less uniform livery in a very bright red: Humbrol 238, which is, probably due to trademark issues, marketed as “Arrow Red (= Red Arrows)” and effectively an almost fluorescent pinkish orange-red! Only the black anti-glare panel in front of the windscreen, the radome and the white interior of the fenestron tail rotor were painted, too, the rest was created with white decal stripes and evolved gradually. Things started with a white 2mm cheatline, then came the horizontal stripes on the tail, and taking this "theme" further I added something similar to the flanks as a high contrast base for the national markings. These were improvised, too, with a 6mm blue disc and single 1.5 mm bars to create a Scottish flag. The stancils were taken from the OOB decal sheet. The interior became medium grey, the crew received bright orange jumpsuits and white "bone domes".

 

No black ink washing or post-panel-shading was done, since the Dauphin has almost no surface details to emphasize, and I wanted a new and clean look. Besides, with wll the white trim, there was already a lot going on on the hull, so that I kept things "as they were". Finally, the model was sealed with a coat of semi-gloss acrylic varnish for a light shine, except for the rotor blades and the anti-glare panel, which became matt.

  

Quite a tricky project. While the Matchbox Dauphin is not a complex kit you need patience and have to stick to the assembly order to put the hull together. PSR is needed, esp. around the engine section and for the underside. On the other side, despite being a simple model, you get a nice Dauphin from the kit - but NOT a HH-65, sorry. My fictional conversion is certainly not better, but the bright result with its modifications looks good and quite convincing, though.

+++ DISCLAIMER +++

Nothing you see here is real, even though the conversion or the presented background story might be based on historical facts. BEWARE!

  

Some Background:

The Lockheed F-94 Starfire was a first-generation jet aircraft of the United States Air Force. It was developed from the twin-seat Lockheed T-33 Shooting Star in the late 1940s as an all-weather, day/night interceptor, replacing the propeller-driven North American F-82 Twin Mustang in this role. The system was designed to overtake the F-80 in terms of performance, but more so to intercept the new high-level Soviet bombers capable of nuclear attacks on America and her Allies - in particular, the new Tupelov Tu-4. The F-94 was furthermore the first operational USAF fighter equipped with an afterburner and was the first jet-powered all-weather fighter to enter combat during the Korean War in January 1953.

 

The initial production model, the F-94A, entered operational service in May 1950. Its armament consisted of four 0.50 in (12.7 mm) M3 Browning machine guns mounted in the fuselage with the muzzles exiting under the radome for the APG-33 radar, a derivative from the AN/APG-3, which directed the Convair B-36's tail guns and had a range of up to 20 miles (32 km). Two 165 US Gallon (1,204 litre) drop tanks, as carried by the F-80 and T-33, were carried on the wingtips. Alternatively, these could be replaced by a pair of 1,000 lb (454 kg) bombs under the wings, giving the aircraft a secondary fighter bomber capability. 109 were produced.

 

The subsequent F-94B, which entered service in January 1951, was outwardly virtually identical to the F-94A. Its Allison J33 turbojet had a number of modifications made, though, which made it a very reliable engine. The pilot was provided with a roomier cockpit and the canopy received a bow frame in the center between the two crew members. A new Instrument Landing System (ILS) was fitted, too, which made operations at night and/or in bad weather much safer. However, this new variant’s punch with just four machine guns remained weak, and, to improve the load of fire, wing-mounted pods with two additional pairs of 0.5” machine guns were introduced – but these hardly improved the interceptor’s effectiveness. 356 of the F-94B were nevertheless built.

 

The following F-94C was extensively modified and initially designated F-97, but it was ultimately decided just to treat it as a new version of the F-94. USAF interest was lukewarm since aircraft technology had already developed at a fast pace – supersonic performance had already become standard. Lockheed funded development themselves, converting two F-94B airframes to YF-94C prototypes for evaluation with a completely new, much thinner wing, a swept tail surface and a more powerful Pratt & Whitney J48. This was a license-built version of the afterburning Rolls-Royce Tay, which produced a dry thrust of 6,350 pounds-force (28.2 kN) and approximately 8,750 pounds-force (38.9 kN) with afterburning. Instead of machine guns, the proposed new variant was exclusively armed with unguided air-to-air missiles.

Tests were positive and eventually the F-94C was adopted for USAF service, since it was the best interim solution for an all-weather fighter at that time. It still had to rely on Ground Control Interception Radar (GCI) sites to vector the interceptor to intruding aircraft, though.

 

The F-94C's introduction and the availability of the more effective Northrop F-89C/D Scorpion and the North American F-86D Sabre interceptors led to a quick relegation of the earlier F-94 variants from mid-1954 onwards to second line units and to Air National Guards. By 1955 most of them had already been phased out of USAF service, and some of these relatively young surplus machines were subsequently exported or handed over to friendly nations, too. When sent to the ANG, the F-94As were modified by Lockheed to F-94B standards and then returned to the ANG as B models. They primarily replaced outdated F-80C Shooting Stars and F-51D/H Mustangs.

 

At that time the USAF was looking for a tactical reconnaissance aircraft, a more effective successor for the RF-80A which had shown its worth and weaknesses during the Korea War. For instance, the plane could not fly at low altitude long enough to perform suitable visual reconnaissance, and its camera equipment was still based on WWII standards. Lockheed saw the opportunity to fill this operational gap with conversions of existing F-94A/B airframes, which had, in most cases, only had clocked few flying hours, primarily at high altitudes where Soviet bombers were expected to lurk, and still a lot of airframe life to offer. This led to another private venture, the RF-94B, auspiciously christened “Stargazer”.

 

The RF-94B was based on the F-94B interceptor with its J33 engine and the original unswept tail. The F-94B’s wings were retained but received a different leading-edge profile to better cope with operations at low altitude. The interceptor’s nose with the radome and the machine guns underneath was replaced by a new all-metal nose cone, which was more than 3 feet longer than the former radar nose, with windows for several sets of cameras; the wedge-shaped nose cone quickly earned the aircraft the unofficial nickname “Crocodile”.

One camera was looking ahead into flight direction and could be mounted at different angled downward (but not moved during flight), followed by two oblique cameras, looking to the left and the right, and a vertical camera as well as a long-range camera focussed on the horizon, which was behind a round window at port side. An additional, spacious compartment in front of the landing gear well held an innovative Tri-Metrogen horizon-to-horizon view system that consisted of three synchronized cameras. Coupled with a computerized control system based on light, speed, and altitude, it adjusted camera settings to produce pictures with greater delineation.

All cameras could be triggered individually by pilot or a dedicated observer/camera systems operator in the 2nd seat. Talking into a wire recorder, the crew could describe ground movements that might not have appeared in still pictures. A vertical view finder with a periscopic presentation on the cockpit panel was added for the pilot to enhance visual reconnaissance and target identification directly under the aircraft. Using magnesium flares carried under its wings in flash-ejector cartridges, the RF-94B was furthermore able to fly night missions.

The RF-94B was supposed to operate unarmed, but it could still carry a pair of 1.000 lb bombs under its wings or, thanks to added plumbings, an extra pair of drop tanks for ferry flights. The F-94A/B’s machine gun pods as well as the F-94C’s unguided missile launchers could be mounted to the wings, too, making it a viable attack aircraft in a secondary role.

 

The USAF was highly interested in this update proposal for the outdated interceptors (almost 500 F-94A/Bs had been built) and ordered 100 RF-94B conversions with an option for 100 more – just when a severe (and superior) competitor entered the stage after a lot of development troubles: Republic’s RF-84F Thunderflash reconnaissance version. The first YRF-84F had already been completed in February 1952 and it had an overall slightly better performance than the RF-94B. However, it offered more internal space for reconnaissance systems and was able to carry up to fifteen cameras with the support of many automatized systems, so that it was a single seater. Being largely identical to the F-84F and sharing its technical and logistical infrastructures, the USAF decided on short notice to change its procurement decision and rather adopt the more modern and promising Thunderflash as its standard tactical reconnaissance aircraft. The RF-94B conversion order was reduced to the initial 100 aircraft, and to avoid operational complexity these aircraft were exclusively delivered to Air National Guardss that had experience with the F-94A/B to replace their obsolete RF-80As.

 

Gradual replacement lasted until 1958, and while the RF-94B’s performance was overall better than the RF-80A’s, it was still disappointing and not the expected tactical intelligence gathering leap forward. The airframe did not cope well with constant low-level operations, and the aircraft’s marginal speed and handling did not ensure its survivability. However, unlike the RF-84F, which suffered from frequent engine problems, the Stargazers’ J33 made them highly reliable platforms – even though the complex Tri-Metrogen device turned out to be capricious, so that it was soon replaced with up to three standard cameras.

 

For better handling and less drag esp. at low altitude, the F-94B’s large Fletcher type wingtip tanks were frequently replaced with smaller ones with about half capacity. It also became common practice to operate the RF-94Bs with only a crew of one, and from 1960 on the RF-94B was, thanks to its second seat, more and more used as a trainer before pilots mounted more potent reconnaissance aircraft like the RF-101 Voodoo, which eventually replaced the RF-94B in ANG service. The last RF-94B was phased out in 1968, and, unlike the RF-84F, it was not operated by any foreign air force.

  

General characteristics:

Crew: 2 (but frequently operated by a single pilot)

Length: 43 ft 4 3/4 in (13.25 m)

Wingspan (with tip tanks): 40 ft 9 1/2 in (12.45 m)

Height: 12 ft. 2 (3.73 m)

Wing area: 234' 8" sq ft (29.11 m²)

Empty weight: 10,064 lb (4,570 kg)

Loaded weight: 15,330 lb (6,960 kg)

Max. takeoff weight: 24,184 lb (10,970 kg)

 

Powerplant:

1× Allison J33-A-33 turbojet, rated at 4,600 lbf (20.4 kN) continuous thrust,

5,400 lbf (24 kN) with water injection and 6,000 lbf (26.6 kN) thrust with afterburner

 

Performance:

Maximum speed: 630 mph (1,014 km/h) at height and in level flight

Range: 930 mi (813 nmi, 1,500 km) in combat configuration with two drop tanks

Ferry range: 1,457 mi (1,275 nmi, 2,345 km)

Service ceiling: 42,750 ft (14,000 m)

Rate of climb: 6,858 ft/min (34.9 m/s)

Wing loading: 57.4 lb/ft² (384 kg/m²)

Thrust/weight: 0.48

 

Armament:

No internal guns; 2x 165 US Gallon (1,204 liter) drop tanks on the wing tips and…

2x underwing hardpoints for two additional 165 US Gallon (1,204 liter) ferry tanks

or bombs of up to 1.000 lb (454 kg) caliber each, plus…

2x optional (rarely fitted) pods on the wings’ leading edges with either a pair of 0.5" (12.7 mm)

machine guns or twelve 2.75” (70 mm) Mk 4/Mk 40 Folding-Fin Aerial Rockets each

  

The kit and its assembly:

This project was originally earmarked as a submission for the 2021 “Reconnaissance & Surveillance” group build at whatifmodellers.com, in the form of a Heller F-94B with a new nose section. The inspiration behind this build was the real-world EF-94C (s/n 50-963): a solitary conversion with a bulbous camera nose. However, the EF-94C was not a reconnaissance aircraft but rather a chase plane/camera ship for the Air Research and Development Command, hence its unusual designation with the suffix “E”, standing for “Exempt” instead of the more appropriate “R” for a dedicated recce aircraft. There also was another EF-94C, but this was a totally different kind of aircraft: an ejection seat testbed.

 

I had a surplus Heller F-94B kit in The Stash™ and it was built almost completely OOB and did – except for some sinkholes and standard PSR work – not pose any problem. In fact, the old Heller Starfire model is IMHO a pretty good representation of the aircraft. O.K., its age might show, but almost anything you could ask for at 1:72 scale is there, including a decent, detailed cockpit.

 

The biggest change was the new camera nose, and it was scratched from an unlikely donor part: it consists of a Matchbox B-17G tail gunner station, slimmed down by the gunner station glazing's width at the seam in the middle, and this "sandwich" was furthermore turned upside down. Getting the transitional sections right took lots of PSR, though, and I added some styrene profiles to integrate the new nose into the rest of the hull. It was unintentional, but the new nose profile reminds a lot of a RF-101 recce Voodoo, and there's, with the straight wings, a very F-89ish look to the aircraft now? There's also something F2H-2ish about the outlines?

 

The large original wing tip tanks were cut off and replaced with smaller alternatives from a Hasegawa A-37. Because it was easy to realize on this kit I lowered the flaps, together with open ventral air brakes. The cockpit was taken OOB, I just modified the work station on the rear seat and replaced the rubber sight protector for the WSO with two screens for a camera operator. Finally, the one-piece cockpit glazing was cut into two parts to present the model with an open canopy.

  

Painting and markings:

This was a tough decision: either an NMF finish (the natural first choice), an overall light grey anti-corrosive coat of paint, both with relatively colorful unit markings, or camouflage. The USAF’s earlier RF-80As carried a unique scheme in olive drab/neutral grey with a medium waterline, but that would look rather vintage on the F-94. I decided that some tactical camouflage would make most sense on this kind of aircraft and eventually settled for the USAF’s SEA scheme with reduced tactical markings, which – after some field tests and improvisations in Vietnam – became standardized and was officially introduced to USAF aircraft around 1965 as well as to ANG units.

 

Even though I had already built a camouflaged F-94 some time ago (a Hellenic aircraft in worn SEA colors), I settled for this route. The basic colors (FS 30219, 34227, 34279 and 36622) all came from Humbrol (118, 117, 116 and 28, respectively), and for the pattern I adapted the paint scheme of the USAF’s probably only T-33 in SEA colors: a trainer based on Iceland during the Seventies and available as a markings option in one of the Special Hobby 1:32 T-33 kits. The low waterline received a wavy shape, inspired by an early ANG RF-101 in SEA camouflage I came across in a book. The new SEA scheme was apparently applied with a lot of enthusiasm and properness when it was brand new, but this quickly vaned. As an extra, the wing tip tanks received black anti-glare sections on their inner faces and a black anti-glare panel was added in front of the windscreen - a decal from a T-33 aftermarket sheet. Beyond a black ink wash the model received some subtle panel post-shading, but rather to emphasize surface details than for serious weathering.

 

The cockpit became very dark grey (Revell 06) while the landing gear wells were kept in zinc chromate green primer (Humbrol 80, Grass Green), with bright red (Humbrol 60, Matt Red) cover interiors and struts and wheels in aluminum (Humbrol 56). The interior of the flaps and the ventral air brakes became red, too.

 

The decals/markings came from a Special Hobby 1:72 F-86H; there’s a dedicated ANG boxing of the kit that comes with an optional camouflaged aircraft of the NY ANG, the least unit to operate the “Sabre Hog” during the Seventies. Since this 138th TFS formerly operated the F-94A/B, it was a perfect option for the RF-94B! I just used a different Bu. No. code on the fin, taken from a PrintScale A/T-37 set, and most stencils were perocured from the scrap box.

After a final light treatment with graphite around the afterburner for a more metallic shine of the iron metallic (Revell 97) underneath, the kit was sealed with a coat of matt acrylic varnish (Italeri).

  

A camouflaged F-94 is an unusual sight, but it works very well. The new/longer nose considerably changes the aircraft's profile, and even though the change is massive, the "Crocodile" looks surprisingly plausible, if not believable! And, despite the long nose, the aircraft looks pretty sleek, especially in the air.

+++ DISCLAIMER +++

Nothing you see here is real, even though the conversion or the presented background story might be based historical facts. BEWARE!

 

Some background:

The Northrop Grumman-IAI F-24 is the latest reincarnation of the USAF "Lightweight Fighter Program" which dates back to the 1950ies and started with the development of Northrop's F-5 "Freedom Fighter".

 

The 1st generation F-5 became very successful in the export market and saw a long line of development, including the much more powerful F-5E "Tiger II" and the F-20 Tigershark (initially called F-5G). Northrop had high hopes for the F-20 in the international market; however, policy changes following Ronald Reagan's election meant the F-20 had to compete for sales against aircraft like the F-16, the USAF's latest fighter design (which was politically favored). The F-20 development program was eventually abandoned in 1986 after three prototypes had been built and a fourth partially completed.

 

But this was not the end for Northrop’s Lightweight Fighter. In the early 1980s, two X-29As experimental aircraft were built by Grumman from two existing Northrop F-5A Freedom Fighter airframes. The Grumman X-29 was a testbed for forward-swept wings, canard control surfaces, and other novel aircraft technologies. The aerodynamic instability of this arrangement increased agility but required the use of computerized fly-by-wire control. Composite materials were used to control the aeroelastic divergent twisting experienced by forward-swept wings, also reducing the weight. The NASA test program continued from 1984 to 1991 and the X-29s flew 242 times, gathering valuable data and breaking ground for new aerodynamic technologies of 4th and 5th generation fighters.

 

Even though no service aircraft directly evolved from the X-29, its innovative FBW system as well as the new material technologies also opened the door for an updated F-20 far beyond the 1990ies. It became clear that ever expensive and complex aircraft could not be the answer to modern, asymmetrical warfare in remote corners of the world, with exploding development costs and just a limited number of aircraft in service that could not generate true economies of scale, esp. when their state-of-the-art design would not permit any export.

Anyway, a global market for simpler fighter aircraft was there, as 1st generation F-16s as well as the worldwide, aging F-5E fleet and types of Soviet/Russian origin like the MiG-29 provided the need for a modern, yet light and economical jet fighter. Contemporary types like the Indian HAL Tejas, the Swedish Saab Gripen, the French Dassault Rafale and the Pakistani/Chinese FC-1/JF-17 ”Thunder” proved this trend among 4th - 4.5th generation fighter aircraft.

 

Northrop Grumman (Northrop bought Grumman in 1994) initiated studies and basic design work on a respective New Lightweight Fighter (NLF) as a private venture in 1995. Work on the NLF started at a slow pace, as the company was busy with re-structuring.

The idea of an updated lightweight fighter was fueled by another source, too: Israel. In 1998 IAI started looking in the USA for a development partner for a new, light fighter that would replace its obsolete Kfir fleet and partly relieve its F-16 and F-15 fleet from interception tasks. The domestic project for that role, the IAI Lavi, had been stillborn, but lots of its avionics and research were still at hand and waited for an airframe for completion.

The new aircraft for the IAF was to be superior to the MiG-29, at least on par with the F-16C/D, but easier to maintain, smaller and overall cheaper. Since the performance profiles appeared to be similar to what Northrop Grumman was developing under the NLF label, the US company eventually teamed up with IAI in 2000 and both started the mutual project "Namer" (=נמר, “Tiger” in Hebrew), which eventually lead to the F-24 I for the IAF which kept its project name for service and to the USAF’s F-24A “Tigershark”.

 

The F-24, as the NLF, was based on the F-20 airframe, but outwardly showed only little family heritage, onle the forward fuselage around the cockpit reminds of the original F-5 design . Many aerodynamic details, e. g. the air intakes and air ducts, were taken over from the X-29, though, as the experimental aircraft and its components had been developed for extreme maneuvers and extra high agility. Nevertheless, the X-29's forward-swept wing was considered to be too exotic and fragile for a true service aircraft, but the F-24 was to feature an Active Aeroelastic Wing (AAW) system.

 

AAW Technology integrates wing aerodynamics, controls, and structure to harness and control wing aeroelastic twist at high speeds and dynamic pressures. By using multiple leading and trailing edge controls like "aerodynamic tabs", subtle amounts of aeroelastic twist can be controlled to provide large amounts of wing control power, while minimizing maneuver air loads at high wing strain conditions or aerodynamic drag at low wing strain conditions. This system was initially tested on the X-29 and later on the X-53 research aircraft, a modified F-18, until 2006.

 

Both USAF and IAF versions feature this state-of-the-art aerodynamic technology, but it is uncertain if other customers will receive it. While details concerning the F-24's system have not been published yet, it is assumed that its AAW is so effective that canard foreplanes could be omitted without sacrificing lift and maneuverability, and that drag is effectively minimized as the wing profile can be adjusted according to the aircraft’s speed, altitude, payload and mission – much like a VG wing, but without its clumsy and heavy swiveling mechanism which has to bear high g forces. As a result, the F-24 is, compared to the F-20, which could carry an external payload of about 3.5 tons, rumored to be able to carry up to 5 tons of ordnance.

 

The delta wing shape proved to be a perfect choice for the required surface and flap actuators inside of the wings, and it would also offer a very good compromise between lift and drag for a wide range of performance. Anyway, there was one price to pay: in order to keep the wing profile thin and simple, the F-24’s landing gear retracts into the lower fuselage, leaving the aircraft with a relatively narrow track.

 

Another major design factor for the outstanding performance of this rather small aircraft was weight reduction and structural integrity – combined with simplicity, ruggedness and a modular construction which would allow later upgrades. Instead of “going big” and expensive, the new F-24 was to create its performance through dedicated loss of weight, which was in some part also a compensation for the AAW system in the wings and its periphery.

 

Weight was saved wherever possible, e .g. a newly developed, lightweight M199A1 gatling gun. This 20mm cannon is a three-barreled, heavily modified version of the already “stripped” M61A2 gun in the USAF’s current F-18E and F-22. One of the novel features is a pneumatic drive instead of the traditional electric mechanism, what not only saves weight but also improves trigger response. The new gun weighs only a mere 65kg (the six-barreled M61A2 weighs 92kg, the original M61A1 112 kg), but still reaches a burst rate of fire of 1.800 RPM (about 800 RPM under cyclic fire, standard practice is to fire the cannon in 30 to 50-round bursts, though) and a muzzle velocity of 1.050 metres per second (3,450 ft/s) with a PGU-28/B round.

 

While the F-16 was and is still made from 80% aluminum alloys and only from 3% composites, the F-24 makes major use of carbon fiber and other lightweight materials, which make up about 40% of the aircraft’s structure, plus an increased share of Titanium and Magnesium alloys. As a consequence and through many other weight-saving measures like keeping stealth capabilities to a minimum (even though RAM was deliberately used and many details designed to have a natural low radar signature, resulting in modest radar cross-section (RCS) reductions), a single, relatively small engine, a fuel-efficient F404-GE-402 turbofan, is enough to make the F-24 a fast and very agile aircraft, coupled with a good range. The F-24’s thrust/weight ratio is considerably higher than 1, and later versions with a vectored thrust nozzle (see below) will take this level of agility even further – with the pilot becoming the limiting factor for the aircraft’s performance.

 

USAF and IAF F-24s are outfitted with Northrop Grumman's AN/APG-80 Active Electronically Scanned Array (AESA) radar, also used in the F-16 Block 60 aircraft. Other customers might only receive the AN/APG-68, making the F-24 comparable to the F-16C/D.

 

The first prototype, the YF-24, flew on 8th of March 2008, followed by two more aircraft plus a static airframe until summer 2010. In early 2011 the USAF placed an initial order of 101 aircraft (probably also to stir export sales – the earlier lightweight fighters from Northrop suffered from the fact that the manufacturer’s country would not use the aircraft in its own forces). These initial aircraft will replace older F-16 in the interceptor role, or free them for fighter bomber tasks. The USN and USMC also showed interest in the aircraft for their aggressor squadrons, for dissimilar air combat training. A two-seater, called the F-24B, is supposed to follow soon, too, and a later version for 2020 onwards, tentatively designated F-24C, is to feature an even stronger F404 engine and a 3D vectoring nozzle.

 

Israel is going to produce its own version domestically from late 2014 on, which will exclusively be used by the IAF. These aircraft will be outfitted with different avionics, built by Elta in Israel, and cater to national requirements which focus more on multi-purpose service, while the USAF focusses with its F-24A on aerial combat and interception tasks.

 

International interest for the F-24A is already there: in late 2013 Grumman stated that initial talks have been made with various countries, and potential export candidates from 2015 on are Taiwan, Singapore, Thailand, Finland, Norway, Australia and Japan.

  

General F-24A characteristics:

Crew: 1 pilot

Length: 47 ft 4 in (14.4 m)

Wingspan: 27 ft 11.9 in / 8.53 m; with wingtip missiles (26 ft 8 in/ 8.13 m; without wingtip missiles)

Height: 13 ft 10 in (4.20 m)

Wing area: 36.55 m² (392 ft²)

Empty weight: 13.150 lb (5.090 kg)

Loaded weight: 15.480 lb (6.830 kg)

Max. take-off weight: 27.530 lb (12.500 kg)

 

Powerplant

1× General Electric F404-GE-402 turbofan with a dry thrust of 11,000 lbf (48.9 kN) and 17,750 lbf (79.2 kN) with afterburner

 

Performance

Maximum speed: Mach 2+

Combat radius: 300 nmi (345 mi, 556 km); for hi-lo-hi mission with 2 × 330 US gal (1,250 L) drop tanks

Ferry range: 1,490 nmi (1715 mi, 2759 km); with 3 × 330 US gal (1,250 L) drop tanks

Service ceiling: 55,000 ft (16,800 m)

Rate of climb: 52,800 ft/min (255 m/s)

Wing loading: 70.0 lb/ft² (342 kg/m²)

Thrust/weight: 1.09 (1.35 with loaded weight & 50% fuel)

 

Armament

1× 20 mm (0.787 in) M199A1 3-barreled Gatling cannon in the lower fuselage with 400 RPG

Eleven external hardpoints (two wingtip tails, six underwing hardpoints, three underfuselage hardpoints) and a total capacity of 11.000 lb (4.994 kg) of missiles (incl. AIM 9 Sidewinder and AIM 120 AMRAAM), bombs, rockets, ECM pods and drop tanks for extended range.

  

The kit and its assembly:

A spontaneous project. This major kitbash was inspired by fellow user nighthunter at whatifmodelers.com, who came up with a profile of a mashed-up US fighter, created “out of boredom”. The original idea was called F-21C, and it was to be a domestic successor to the IAI Kfirs which had been used by the US as aggressor aircraft in USN and USMC service for a few years.

 

As a weird(?) coincidence I had many of the necessary ingredients for this fictional aircraft in store, even though some parts and details were later changed. This model here is an interpretation of the original design. The idea was spun further, and the available parts that finally went into the model also had some influence on design and background.

I thank nighthunter for sharing the early ideas, inviting me to take the design to the hardware stage (sort of…) and adapting my feedback into new design sketches, too, which, in return, inspired the model building process.

 

Well, what went into this thing? To cook up a F-24 à la Dizzyfugu you just need (all in 1:72):

● Fuselage from a Hasegawa X-29, including the cockpit and the landing gear

● Fin and nose cone from an Italeri F-16A

● Inner wings from a (vintage) Hasegawa MiG-21F

● Outer wings from a F-4 (probably a J, Hasegawa or Fujimi)

 

The wing construction deviates from nighthunter’s original idea. The favorite ingredients would have been F-16XL or simple Mirage III wings, but I found the composite wing to be more attractive and “different”. The big F-16XL wings, despite their benefit of a unique shape, might also have created scale/size problems with a F-20 style fuselage? So I built hybrid wings: The MiG-21 landing gear wells were filled with putty and the F-4 outer wings simply glued onto the MiG inner wing sections, which were simply cut down in span. It sounds like an unlikely combo, but these parts fit together almost perfectly! In order to hide the F-4 origins I modified them to carry wingtip launch rails, though, which were also part of nighthunter’s original design.

 

The AAW technology detail mentioned in the background came in handy as it explains the complicated wing shape and the fact that the landing gear retracts into the fuselage, not into the wings, which would have been more plausible… Anyway, there’s still room for a simpler export version, with Mirage III or Kfir C.2/7 wings, and maybe canards?

 

Using the X-29 as basis also made fitting the new wings onto the area-ruled fuselage pretty easy, as I could use the wing root parts from the X-29 to bridge the gap. The original, forward-swept wings were just cut away, and the remains used as consoles for the new hybrid delta wings. Took some SERIOUS putty work, but the result is IMHO fine.

 

The bigger/square X-29 air intakes were taken over, and they change the look of the aircraft, making it look less F-5-ish than a true F-20 fuselage. For the same reason I kept the large fairing at the fin base, combining it with a bigger F-16 tail, though, as a counter-balance to the new, bigger wings. Again, the F-16 fin was/is part of nighthunter’s idea, so the model stays true to the original concept.

 

For the same reason I omitted the original X-29 nose, which is rather pointy, sports vanes and a large sensor boom. The F-16 nose was a plausible choice, as the AN/APG-80 is also carried by late Fighting Falcons, and its shape fits well, too.

 

All around the hull, some small details like radar warning sensors, pitots and air scoops were added. Not really necessary, but such thing add IMHO to the overall impression of such a fictional aircraft beyond the prototype stage.

 

Cockpit and landing gear were taken OOB, I just added a pilot figure and slightly modified the seat.

 

The ordnance was puzzled together from the scrap box, the AIM-9Ls come from the same F-4 kit which donated its outer wings, the AIM-120s come from an Italeri NATO weapons kit. The drop tanks belong to an F-16.

  

Painting and markings:

At first I considered an F-24I in IAF markings, or even a Japanese aircraft, but then reverted to one of nighthunter’s initial, simple ideas: an USAF aircraft in the “Hill II” paint scheme (F-16 style), made up from three shades of gray (FS 36118, 36270 and 36375) with low-viz markings and stencils. Dutch/Turkish NF-5A/Bs in the “Hill II” scheme were used as design benchmarks, too. It’s a simple livery, but on this delta wing aircraft it looks pretty interesting. I used enamels, what I had at hand: Humbrol 127 and 126, and Modelmaster's 1723.

 

A light black ink wash was applied, in order to em,phasize the engraved panel lines, in contrast to that, panels were manually highlighted through dry-brushed, lighter shades of gray (Humbrol 27, 166 and 167).

 

“Hill II” also adds to a generic, realistic touch for this whif. Doing an exotic air force thing is rather easy, but creating a convincing whif for a huge military machinery like the USAF’s takes more subtlety, I think.

 

The cockpit was painted in medium Gray (Dark Gull Grey, FS 36231, Humbrol 140), as well as the radome. The landing gear and the air intakes were painted white. The radome was painted with Revell 47 and dry-brushed with Humbrol 140.

 

Decals were puzzled together from various USAF aircraft, including sheets from an Airfix F-117, an Italeri F-15E and even an Academy OV-10D.

  

Tadah: a hardware tribute to an idea, born from boredom - and the aircraft does not look even bad at all? What I wanted to achieve was to make the F-24 neither look like a F-20, nor a Saab Gripen clone, as the latter comes close in overall shape, size and design.

Western section of the San Francisco- Oakland Bay bridge. Connecting to Yerba Buena Island on the left.

Public light show installation (2013)

On March 5, 2013, a public art installation called "The Bay Lights" was activated on the western span's vertical cables. The installation was designed by artist Leo Villareal and consists of 25,000 LED lights. It will be on display nightly until 2015.[36] In order to reduce driver distractions, the privately funded display is not visible to users of the bridge, only to distant observers. This lighting effort is intended to form part of a larger project to "light the bay"[37] Villareal used various algorithms to generate patterns such as rainfall, reflections on water, bird flight, expanding rings, and others. Villareal's patterns and transitions will be sequenced and their duration determined by computerized random number generator to make each viewing experience unique.[38] Owing to the efficiency of the LED system the estimated operating cost is only US $15.00 per night.

 

All rights reserved - Copyright 2014© Henri Louis Hirschfeld

All images are exclusive property and may not be copied, downloaded, reproduced, transmitted, manipulated or used in any way without expressed, written permission of the photographer.

Parked trailer full of crushed cars ready for their final journey to the recycling plant.

A wrecking yard (Australian, New Zealand, and Canadian English), scrapyard (Irish and British English) or junkyard (American English) is the location of a business in dismantling where wrecked or decommissioned vehicles are brought, their usable parts are sold for use in operating vehicles, while the unusable metal parts, known as scrap metal parts, are sold to metal-recycling companies.

 

Other terms include wreck yard, wrecker's yard, salvage yard, breakers yard, dismantler and scrapheap. In the United Kingdom, car salvage yards are known as car breakers, while motorcycle salvage yards are known as bike breakers. In Australia, they are often referred to as 'Wreckers'.

 

The most common type of wreck yards are automobile wreck yards, but junkyards for motorcycles, bicycles, small airplanes and boats exist too.

 

Many salvage yards operate on a local level—when an automobile is severely damaged, has malfunctioned beyond repair, or not worth the repair, the owner may sell it to a junkyard; in some cases—as when the car has become disabled in a place where derelict cars are not allowed to be left—the car owner will pay the wrecker to haul the car away.

 

Salvage yards also buy most of the wrecked, derelict and abandoned vehicles that are sold at auction from police impound storage lots,and often buy vehicles from insurance tow yards as well.

 

The salvage yard will usually tow the vehicle from the location of its purchase to the yard, but occasionally vehicles are driven in. At the salvage yard the automobiles are typically arranged in rows, often stacked on top of one another.

 

Some yards keep inventories in their offices, as to the usable parts in each car, as well as the car's location in the yard. Many yards have computerized inventory systems. About 75% of any given vehicle can be recycled and used for other goods.

 

In recent years it is becoming increasingly common to use satellite part finder services to contact multiple salvage yards from a single source.

 

In the 20th century these were call centres that charged a premium rate for calls and compiled a facsimile that was sent to various salvage yards so they could respond directly if the part was in stock. Many of these are now Web-based with requests for parts being e-mailed instantly.

+++ DISCLAIMER +++

Nothing you see here is real, even though the conversion or the presented background story might be based on historical facts. BEWARE!

  

Some background:

The ZSU-37-6 (“ZSU” stands for Zenitnaya Samokhodnaya Ustanovka / Зенитная Самоходная Установка = "anti-aircraft self-propelled mount"), also known as Object 511 during its development phase and later also as “ZSU-37-6 / Лена”, was a prototype for a lightly armored Soviet self-propelled, radar guided anti-aircraft weapon system that was to replace the cannon-armed ZSU-23-4 “Shilka” SPAAG.

The development of the "Shilka" began in 1957 and the vehicle was brought into service in 1965. The ZSU-23-4 was intended for AA defense of military facilities, troops, and mechanized columns on the march. The ZSU-23-4 combined a proven radar system, the non-amphibious chassis based on the GM-575 tracked vehicle, and four 23 mm autocannons. This delivered a highly effective combination of mobility with heavy firepower and considerable accuracy, outclassing all NATO anti-aircraft guns at the time. The system was widely fielded throughout the Warsaw Pact and among other pro-Soviet states. Around 2,500 ZSU-23-4s, of the total 6,500 produced, were exported to 23 countries.

 

The development of a potential successor started in 1970. At the request of the Soviet Ministry of Defense, the KBP Instrument Design Bureau in Tula started work on a new mobile anti-aircraft system as a replacement for the 23mm ZSU-23-4. The project was undertaken to improve on the observed shortcomings of the ZSU-23-4 (short range and no early warning) and to counter new ground attack aircraft in development, such as the A-10 Thunderbolt II, which was designed to be highly resistant to 23 mm cannons.

 

KBP studies demonstrated that a cannon of at least 30 mm caliber was necessary to counter these threats, and that a bigger caliber weapon would offer some more benefits. Firstly, to destroy a given target, such a weapon would only require from a third to a half of the number of shells that the ZSU-23-4’s 23 mm cannon would need. Secondly, comparison tests revealed that firing with an identical mass of 30 mm projectiles instead of 23 mm ammunition at a MiG-17 (or similarly at NATO's Hawker Hunter or Fiat G.91…) flying at 300 m/s would result in a 1.5 times greater kill probability. An increase in the maximum engagement altitude from 2,000 to 4,000 m and higher effectiveness when engaging lightly armored ground targets were also cited as potential benefits.

 

The initial requirements set for the new mobile weapon system were to achieve twice the performance in terms of the ZSU-23-4’s range, altitude and combat effectiveness. Additionally, the system should have a reaction time, from target acquisition to firing, no greater than 10 seconds, so that enemy helicopters that “popped up” from behind covers and launched fire-and-forget weapons at tanks or similar targets could be engaged effectively.

From these specifications KBP developed two schools of thought that proposed different concepts and respective vehicle prototypes: One design team followed the idea of an anti-aircraft complex with mixed cannon and missile armament, which made it effective against both low and high-flying targets but sacrificed short-range firepower. The alternative proposed by another team was a weapon carrier armed only with a heavy gatling-type gun, tailored to counter targets flying at low altitudes, esp. helicopters, filling a similar niche as the ZSU-23-4 and leaving medium to high altitude targets to specialized anti-aircraft missiles. The latter became soon known as “Object 511”.

 

Object 511 was based on the tracked and only lightly armored GM-577 chassis, produced by Minsk Tractor Works (MTZ). It featured six road wheels on each side, a drive sprocket at the rear and three return rollers. The chassis was primarily chosen because it was already in use for other anti-aircraft systems like the 2K11 “Krug” complex and could be taken more or less “off the rack”. A new feature was a hydropneumatic suspension, which was chosen in order to stabilize the chassis as firing platform and also to cope with the considerably higher all-up weight of the vehicle (27 tons vs. the ZSU-23-4’s 19 tons). Other standard equipment of Object 511 included heating, ventilation, navigational equipment, night vision aids, a 1V116 intercom and an external communications system with an R-173 receiver.

 

The hull was - as the entire vehicle - protected from small arms fire (7,62mm) and shell splinters, but not heavily armored. An NBC protection system was integrated into the chassis, as well as an automatic fire suppression system and an automatic gear change. The main engine bay, initially with a 2V-06-2 water-cooled multi-fuel diesel engine with 450 hp (331 kW) was in the rear. It was later replaced by a more powerful variant of the same engine with 510 hp (380 kW).

The driver sat in the front on the left side, with a small gas turbine APU to his right to operate the radar and hydraulic systems independently from the main engine.

Between these hull segments, the chassis carried a horseshoe-shaped turret with full 360° rotation. It was relatively large and covered more than the half of the hull’s roof, because it held the SPAAGs main armament and ammunition supply, the search and tracking radar equipment as well as a crew of two: the commander with a cupola on the right side and the gunner/radar operator on the left side, with the cannon installation and its feeding system between them. In fact, it was so large that Object 511’s engine bay was only accessible when the turret was rotated 90° to the side – unacceptable for an in-service vehicle (which would probably have been based on a bigger chassis), but accepted for the prototype which was rather focused on the turret and its complex weapon and radar systems.

 

Object 511’s centerpiece was the newly-developed Gryazev-Shipunov GSh-6-37 cannon, a heavy and experimental six-barreled 37mm gatling gun. This air-cooled weapon with electrical ignition was an upscaled version of the naval AO-18 30mm gun, which was part of an automated air defense system for ships, the AK-630 CIWS complex. Unlike most modern American rotary cannons, the GSh-6-37 was gas-operated rather than hydraulically driven, allowing it to "spin up" to maximum rate of fire more quickly. This resulted in more rounds and therefore weight of fire to be placed on target in a short burst, reduced reaction time and allowed hits even in a very small enemy engagement window.

 

The GSh-6-37 itself weighed around 524 kg (1.154 lb), the whole system, including the feed system and a full magazine, weighed 7,493 pounds (3,401 kg). The weapon had a total length of 5.01 m (16’ 7“), its barrels were 2.81 m (9’ 2½”) long. In Object 511’s turret it had an elevation between +80° and -11°, moving at 60°/sec, and a full turret rotation only took 3 seconds. Rate of fire was 4,500 rounds per minute, even though up to 5.500 RPM were theoretically possible and could be cleared with an emergency setting. However, the weapon would typically only fire short bursts of roundabout 50 rounds each, or longer bursts of 1-2 (maximum) seconds to save ammunition and to avoid overheating and damage – initially only to the barrels, but later also to avoid collateral damage from weapon operation itself (see below). Against ground targets and for prolonged, safe fire, the rate of fire could alternatively be limited to 150 RPM.

The GSh-6-37 fired 1.09 kg shells (each 338mm long) at 1,070 m/s (3.500 ft/s), developing a muzzle energy of 624,000 joules. This resulted in an effective range of 6,000 m (19.650 ft) against aerial and 7,000 m (23.0000 ft) against ground targets. Maximum firing range was past 7,160 m (23,490 ft), with the projectiles self-destructing beyond that distance. In a 1 sec. burst, the weapon delivered an impressive weight of fire of almost 100 kg.

The GSh-6-37 was belt-fed, with a closed-circuit magazine to avoid spilling casings all around and hurting friendly troops in the SPAAG’s vicinity. Typical types of ammunition were OFZT (proximity-fused incendiary fragmentation) and BZT (armor-piercing tracer, able to penetrate more than 60 mm of 30° sloped steel armor at 1.000 m/3.275’ distance). Since there was only a single ammunition supply that could not be switched, these rounds were normally loaded in 3:1 ratio—three OFZT, then one BZT, every 10th BZT round marked with a tracer. Especially the fragmentation rounds dealt extensive collateral damage, as the sheer numbers of fragments from detonating shells was sufficient to damage aircraft flying within a 200-meter radius from the impact center. This, coupled with the high density of fire, created a very effective obstacle for aerial targets and ensured a high hit probability even upon a casual and hurried attack.

 

The gun was placed in the turret front’s center, held by a massive mount with hydraulic dampers. The internal ammunition supply in the back of the turret comprised a total of 1.600 rounds, but an additional 800 rounds could be added in an external reserve feed bin, attached to the back of the turret and connected to the internal belt magazine loop through a pair of ports in the turret’s rear, normally used to reload the GSh-6-37.

 

A rotating, electronically scanned E-band (10 kW power) target acquisition radar array was mounted on the rear top of the turret that, when combined with the turret front mounted J-band (150 kW power) mono-pulse tracking radar, its dish antenna hidden under a fiberglass fairing to the right of the main weapon, formed the 1RL144 (NATO: Hot Shot) pulse-Doppler 3D radar system. Alongside, the 1A26 digital computer, a laser rangefinder co-axial to the GSh-6-37, and the 1G30 angle measurement system formed the 1A27 targeting complex.

Object 511’s target acquisition offered a 360-degree field of view, a detection range of around 18 km and could detect targets flying as low as 15 m. The array could be folded down and stowed when in transit, lying flat on the turret’s roof. The tracking radar had a range of 16 km, and a C/D-band IFF system was also fitted. The radar system was highly protected against various types of interference and was able to work properly even if there were mountains on the horizon, regardless of the background. The system made it possible to fire the GSh-6-37 on the move, against targets with a maximum target speed of up to 500 m/s, and it had an impressive reaction time of only 6-8 seconds.

Thanks to its computerized fire control system, the 1A27 was highly automated and reduced the SPAAG’s crew to only three men, making a dedicated radar operator (as on the ZSU-23-4) superfluous and saving internal space in the large but still rather cramped turret.

 

Development of Object 511 and its systems were kicked-off in 1972 but immediately slowed down with the introduction of the 9K33 “Osa” missile system, which seemed to fill the same requirement but with greater missile performance. However, after some considerable debate it was felt that a purely missile-based system would not be as effective at dealing with very low flying attack helicopters attacking at short range with no warning, as had been proven so successful in the 1973 Arab-Israeli War. Since the reaction time of a gun system was around 8–10 seconds, compared to approximately 30 seconds for a missile-based system, development of Object 511 was restarted in 1973.

 

A fully functional prototype, now officially dubbed “ZSU-37-6“ to reflect its role and armament and christened “Лена” (Lena, after the Russian river in Siberia), was completed in 1975 at the Ulyanovsk Mechanical Factory, but it took until 1976 that the capricious weapon and the 1A27 radar system had been successfully integrated and made work. System testing and trials were conducted between September 1977 and December 1978 on the Donguzskiy range, where the vehicle was detected by American spy satellites and erroneously identified as a self-propelled artillery system with a fully rotating turret (similar to the American M109), as a potential successor for the SAU-122/2S1 Gvozdika or SAU-152/2S3 Akatsiya SPGs that had been introduced ten years earlier, with a lighter weapon of 100-120mm caliber and an autoloader in the large turret.

 

The tests at Donguzskiy yielded mixed results. While the 1A27 surveillance and acquisition radar complex turned out to be quite effective, the GSh-6-37 remained a constant source of problems. The gun was highly unreliable and afforded a high level of maintenance. Furthermore, it had a massive recoil of 6.250 kp/61 kN when fired (the American 30 mm GAU-8 Avenger “only” had a recoil of 4.082 kp/40 kN). As a result, targets acquired by the 1A27 system were frequently lost after a single burst of fire, so that they had to be tracked anew before the next shot could be placed.

To make matters even words, the GSh-6-37 was noted for its high and often uncomfortable vibration and extreme noise, internally and externally. Pressure shock waves from the gun muzzles made the presence of unprotected personnel in the weapon’s proximity hazardous. The GSh-6-37’s massive vibrations shook the whole vehicle and led to numerous radio and radar system failures, tearing or jamming of maintenance doors and access hatches and the cracking of optical sensors. The effects were so severe that the gun’s impact led after six months to fatigue cracks in the gun mount, the welded turret hull, fuel tanks and other systems. One spectacular and fateful showcase of the gun’s detrimental powers was a transmission failure during a field test/maneuver in summer 1978 – which unfortunately included top military brass spectators and other VIPs, who were consequently not convinced of the ZSU-37-6 and its weapon.

 

The GSh-6-37’s persisting vibration and recoil problems, as well as its general unreliability if it was not immaculately serviced, could not be satisfactorily overcome during the 2 years of state acceptance trials. Furthermore, the large and heavy turret severely hampered Object 511’s off-road performance and handling, due to the high center of gravity and the relatively small chassis, so that the weapon system’s full field potential could not be explored. Had it found its way into a serial production vehicle, it would certainly have been based on a bigger and heavier chassis, e.g. from an MBT. Other novel features tested with Object 511, e.g. the hydropneumatic suspension and the automated 1A27 fire control system, proved to be more successful.

 

However, the troublesome GSh-6-37 temporarily attained new interest in 1979 through the Soviet Union’s engagement in Afghanistan, because it became quickly clear that conventional battle tanks, with long-barreled, large caliber guns and a very limited lift angle were not suited against small targets in mountainous regions and for combat in confined areas like narrow valleys or settlements. The GSh-6-37 appeared as a promising alternative weapon, and plans were made to mount it in a more strongly armored turret onto a T-72 chassis. A wooden mockup turret was built, but the project was not proceeded further with. Nevertheless, the concept of an armored support vehicle with high firepower and alternative armament would persist and lead, in the course of the following years, to a number of prototypes that eventually spawned the BMPT "Terminator" Tank Support Fighting Vehicle.

 

More tests and attempts to cope with the gun mount continued on a limited basis through 1979, but in late 1980 trials and development of Object 511 and the GSh-6-37 were stopped altogether: the 2K22 “Tunguska” SPAAG with mixed armament, developed in parallel, was preferred and officially accepted into service. In its original form, the 2K22 was armed with four 9M311 (NATO: SA-19 “Grison”) short-range missiles in the ready-to-fire position and two 2A38 30mm autocannons, using the same 1A27 radar system as Object 511. The Tunguska entered into limited service from 1984, when the first batteries, now armed with eight missiles, were delivered to the army, and gradually replaced the ZSU-23-4.

 

Having become obsolete, the sole Object 511 prototype was retired in 1981 and mothballed. It is today part of the Military Technical Museum collection at Ivanovskaya, near Moscow, even though not part of the public exhibition and in a rather derelict state, waiting for restoration and eventual display.

  

Specifications:

Crew: Three (commander, gunner, driver)

Weight: about 26,000 kg (57,300 lb)

Length: 7.78 m (25 ft 5 1/2 in) with gun facing forward

6.55 m (21 ft 5 1/2 in) hull only

Width: 3.25 m (10 ft 8 in)

Height: 3.88 m (12 ft 9 in) overall,

2.66 m (8 8 1/2 ft) with search radar stowed

Suspension: Hydropneumatic

Ground clearance: 17–57 cm

Fuel capacity: 760 l (200 US gal, 170 imp gal)

 

Armor:

Unknown, but probably not more than 15 mm (0.6”)

 

Performance:

Speed: 65 km/h (40 mph) maximum on the road

Climbing ability: 0.7 m (2.3')

Maximum climb gradient: 30°

Trench crossing ability: 2.5 m (8.2')

Fording depth: 1.0 m (3.3')

Operational range: 500 km (310 mi)

Power/weight: 24 hp/t

 

Engine:

1× 2V-06-2S water-cooled multi-fuel diesel engine with 510 hp (380 kW)

1× auxiliary DGChM-1 single-shaft gas turbine engine with 70 hp at 6,000 rpm,

connected with a direct-current generator

 

Transmission:

Hydromechanical

 

Armament:

1× GSh-6-37 six-barreled 37mm (1.5 in) Gatling gun with 1.600 rounds,

plus 800 more in an optional, external auxiliary magazine

  

The kit and its assembly:

This fictional SPAAG was intended as a submission to the “Prototypes” group build at whatifmodellers.com in August 2020. Inspiration came from a Trumpeter 1:72 2P25/SA-6 launch platform which I had recently acquired with a kit lot – primarily because of the chassis, which would lend itself for a conversion into “something else”.

 

The idea to build an anti-aircraft tank with a gatling gun came when I did research for my recent YA-14 build and its armament. When checking the American GAU-8 cannon from the A-10 I found that there had been plans to use this weapon for a short-range SPAAG (as a replacement for the US Army’s M163), and there had been plans for even heavier weapons in this role. For instance, there had been the T249 “Vigilante” prototype: This experimental system consisted of a 37 mm T250 six-barrel Gatling gun, mounted on a lengthened M113 armored personnel carrier platform, even though with a very limited ammunition supply, good only for 5 sec. of fire – it was just a conceptual test bed. But: why not create a Soviet counterpart? Even more so, since there is/was the real-world GSh-6-30 gatling gun as a potential weapon, which had, beyond use in the MiG-27, also been used in naval defense systems. Why not use/create an uprated/bigger version, too?

 

From this idea, things evolved in a straightforward fashion. The Trumpeter 2P25 chassis and hull were basically taken OOB, just the front was modified for a single driver position. However, the upper hull had to be changed in order to accept the new, large turret instead of the triple SA-6 launch array.

 

The new turret is a parts combination: The basis comes from a Revell 1:72 M109 howitzer kit, the 155 mm barrel was replaced with a QuickBoost 1:48 resin GSh-6-30 gun for a MiG-27, and a co-axial laser rangefinder (a piece of styrene) was added on a separate mount. Unfortunately, the Revell kit does not feature a movable gun barrel, so I decided to implant a functional joint, so that the model’s weapon could be displayed in raised and low position – primarily for the “action pictures”. The mechanism was scratched from styrene tubes and a piece of foamed plastic as a “brake” that holds the weapon in place and blocks the view into the turret from the front when the weapon is raised high up. The hinge was placed behind the OOB gun mantle, which was cut into two pieces and now works as in real life.

Further mods include the dish antenna for the tracking radar (a former tank wheel), placed on a disc-shaped pedestal onto the turret front’s right side, and the retractable rotating search radar antenna, scratched from various bits and pieces and mounted onto the rear of the turret – its roof had to be cleaned up to make suitable space next to the commander’s cupola.

 

Another challenge was the adaptation of the new turret to the hull, because the original SA-6 launch array has only a relatively small turret ring, and it is placed relatively far ahead on the hull. The new, massive turret had to be mounted further backwards, and the raised engine cowling on the back of the hull did not make things easier.

As a consequence, I had to move the SA-6 launcher ring bearing backwards, through a major surgical intervention in the hull roof (a square section was cut out, shortened, reversed and glued back again into the opening). In order to save the M109’s turret ring for later, I gave it a completely new turret floor and transplanted the small adapter ring from the SA-6 launch array to it. Another problem arose from the bulged engine cover: it had to be replaced with something flat, otherwise the turret would not have fitted. I was lucky to find a suitable donor in the spares box, from a Leopard 1 kit. More complex mods than expected, and thankfully most of the uglier changes are hidden under the huge turret. However, Object 511 looks pretty conclusive and menacing with everything in place, and the weapon is now movable in two axis’. The only flaw is a relatively wide gap between the turret and the hull, due to a step between the combat and engine section and the relatively narrow turret ring.

  

Painting and markings:

AFAIK, most Soviet tank prototypes in the Seventies/Eighties received a simple, uniform olive green livery, but ,while authentic, I found this to look rather boring. Since my “Object 511” would have taken part in military maneuvers, I decided to give it an Eighties Soviet Army three-tone camouflage, which was introduced during the late Eighties. It consisted of a relatively bright olive green, a light and cold bluish grey and black-grey, applied in large patches.

This scheme was also adapted by the late GDR’s Volksarmee (called “Verzerrungsanstrich” = “Distortion scheme”) and maybe – even though I am not certain – this special paint scheme might only have been used by Soviet troops based on GDR soil? However, it’s pretty unique and looks good, so I adapted it for the model.

 

Based upon visual guesstimates from real life pictures and some background info concerning NVA tank paint schemes, the basic colors became Humbrol 86 (Light Olive Green; RAL 6003), Revell 57 (Grey; RAL 7000) and Revell 06 (Tar Black; RAL 9021). Each vehicle had an individual paint scheme, in this case it was based on a real world NVA lorry.

 

On top of the basic colors, a washing with a mix of red brown and black acrylic paint was applied, and immediately dried with a soft cotton cloth so that it only remained in recesses and around edges, simulating dirt and dust. Some additional post-shading with lighter/brighter versions of the basic tones followed.

Decals came next – the Red Stars were a rather dramatic addition and came from the Trumpeter kit’s OOB sheet. The white “511” code on the flanks was created with white 3 mm letters from TL Modellbau.

 

The model received a light overall dry brushing treatment with light grey (Revell 75). As a finishing touch I added some branches as additional camouflage. These are bits of dried moss (collected on the local street), colorized with simple watercolors and attached with white glue. Finally, everything was sealed and stabilized with a coat of acrylic matt varnish and some pigments (a greyish-brown mix of various artist mineral pigments) were dusted into the running gear and onto the lower hull surfaces with a soft brush.

  

An effective kitbashing, and while mounting the different turret to the hull looks simple, the integration of unrelated hull and turret so that they actually fit and “work” was a rather fiddly task, and it’s effectively not obvious at all (which is good but “hides” the labour pains related to the mods). However, the result looks IMHO good, like a beefed-up ZSU-23-4 “Schilka”, just what this fictional tank model is supposed to depict.

Two Lockheed Martin F-35B Lightning II fighter jets have successfully landed on board HMS Queen Elizabeth for the first time, laying the foundations for the next 50 years of fixed wing aviation in support of the UK’s Carrier Strike Capability.

 

Royal Navy Commander, Nathan Gray, 41, made history by being the first to land on board HMS Queen Elizabeth, carefully maneuvering his stealth jet onto the thermal coated deck. He was followed by Squadron Leader Andy Edgell, RAF, both of whom are test pilots, operating with the Integrated Test Force (ITF) based at Naval Air Station Patuxent River, Maryland.

 

Shortly afterwards, once a deck inspection has been conducted and the all-clear given, Cmdr Gray became the first pilot to take off using the ship’s ski-ramp.

  

From Wikipedia, the free encyclopedia

 

The Lockheed Martin F-35 Lightning II is a family of single-seat, single-engine, all-weather, stealth, fifth-generation, multirole combat aircraft, designed for ground-attack and air-superiority missions. It is built by Lockheed Martin and many subcontractors, including Northrop Grumman, Pratt & Whitney, and BAE Systems.

 

The F-35 has three main models: the conventional takeoff and landing F-35A (CTOL), the short take-off and vertical-landing F-35B (STOVL), and the catapult-assisted take-off but arrested recovery, carrier-based F-35C (CATOBAR). The F-35 descends from the Lockheed Martin X-35, the design that was awarded the Joint Strike Fighter (JSF) program over the competing Boeing X-32. The official Lightning II name has proven deeply unpopular and USAF pilots have nicknamed it Panther, instead.

 

The United States principally funds F-35 development, with additional funding from other NATO members and close U.S. allies, including the United Kingdom, Italy, Australia, Canada, Norway, Denmark, the Netherlands, and formerly Turkey. These funders generally receive subcontracts to manufacture components for the aircraft; for example, Turkey was the sole supplier of several F-35 parts until its removal from the program in July 2019. Several other countries have ordered, or are considering ordering, the aircraft.

 

As the largest and most expensive military program ever, the F-35 became the subject of much scrutiny and criticism in the U.S. and in other countries. In 2013 and 2014, critics argued that the plane was "plagued with design flaws", with many blaming the procurement process in which Lockheed was allowed "to design, test, and produce the F-35 all at the same time," instead of identifying and fixing "defects before firing up its production line". By 2014, the program was "$163 billion over budget [and] seven years behind schedule". Critics also contend that the program's high sunk costs and political momentum make it "too big to kill".

 

The F-35 first flew on 15 December 2006. In July 2015, the United States Marines declared its first squadron of F-35B fighters ready for deployment. However, the DOD-based durability testing indicated the service life of early-production F-35B aircraft is well under the expected 8,000 flight hours, and may be as low as 2,100 flight hours. Lot 9 and later aircraft include design changes but service life testing has yet to occur. The U.S. Air Force declared its first squadron of F-35As ready for deployment in August 2016. The U.S. Navy declared its first F-35Cs ready in February 2019. In 2018, the F-35 made its combat debut with the Israeli Air Force.

 

The U.S. stated plan is to buy 2,663 F-35s, which will provide the bulk of the crewed tactical airpower of the U.S. Air Force, Navy, and Marine Corps in coming decades. Deliveries of the F-35 for the U.S. military are scheduled until 2037 with a projected service life up to 2070.

 

Development

 

F-35 development started in 1992 with the origins of the Joint Strike Fighter (JSF) program and was to culminate in full production by 2018. The X-35 first flew on 24 October 2000 and the F-35A on 15 December 2006.

 

The F-35 was developed to replace most US fighter jets with the variants of a single design that would be common to all branches of the military. It was developed in co-operation with a number of foreign partners, and, unlike the F-22 Raptor, intended to be available for export. Three variants were designed: the F-35A (CTOL), the F-35B (STOVL), and the F-35C (CATOBAR). Despite being intended to share most of their parts to reduce costs and improve maintenance logistics, by 2017, the effective commonality was only 20%. The program received considerable criticism for cost overruns during development and for the total projected cost of the program over the lifetime of the jets.

 

By 2017, the program was expected to cost $406.5 billion over its lifetime (i.e. until 2070) for acquisition of the jets, and an additional $1.1 trillion for operations and maintenance. A number of design deficiencies were alleged, such as: carrying a small internal payload; performance inferior to the aircraft being replaced, particularly the F-16; lack of safety in relying on a single engine; and flaws such as the vulnerability of the fuel tank to fire and the propensity for transonic roll-off (wing drop). The possible obsolescence of stealth technology was also criticized.

  

Design

 

Overview

 

Although several experimental designs have been developed since the 1960s, such as the unsuccessful Rockwell XFV-12, the F-35B is to be the first operational supersonic STOVL stealth fighter. The single-engine F-35 resembles the larger twin-engined Lockheed Martin F-22 Raptor, drawing design elements from it. The exhaust duct design was inspired by the General Dynamics Model 200, proposed for a 1972 supersonic VTOL fighter requirement for the Sea Control Ship.

 

Lockheed Martin has suggested that the F-35 could replace the USAF's F-15C/D fighters in the air-superiority role and the F-15E Strike Eagle in the ground-attack role. It has also stated the F-35 is intended to have close- and long-range air-to-air capability second only to that of the F-22 Raptor, and that the F-35 has an advantage over the F-22 in basing flexibility and possesses "advanced sensors and information fusion".

 

Testifying before the House Appropriations Committee on 25 March 2009, acquisition deputy to the assistant secretary of the Air Force, Lt. Gen. Mark D. "Shack" Shackelford, stated that the F-35 is designed to be America's "premier surface-to-air missile killer, and is uniquely equipped for this mission with cutting-edge processing power, synthetic aperture radar integration techniques, and advanced target recognition".

 

Improvements

Ostensible improvements over past-generation fighter aircraft include:

 

Durable, low-maintenance stealth technology, using structural fiber mat instead of the high-maintenance coatings of legacy stealth platforms

Integrated avionics and sensor fusion that combine information from off- and on-board sensors to increase the pilot's situational awareness and improve target identification and weapon delivery, and to relay information quickly to other command and control (C2) nodes

High-speed data networking including IEEE 1394b and Fibre Channel (Fibre Channel is also used on Boeing's Super Hornet.

The Autonomic Logistics Global Sustainment, Autonomic Logistics Information System (ALIS), and Computerized maintenance management system to help ensure the aircraft can remain operational with minimal maintenance manpower The Pentagon has moved to open up the competitive bidding by other companies. This was after Lockheed Martin stated that instead of costing 20% less than the F-16 per flight hour, the F-35 would actually cost 12% more. Though the ALGS is intended to reduce maintenance costs, the company disagrees with including the cost of this system in the aircraft ownership calculations. The USMC has implemented a workaround for a cyber vulnerability in the system. The ALIS system currently requires a shipping-container load of servers to run, but Lockheed is working on a more portable version to support the Marines' expeditionary operations.

Electro-hydrostatic actuators run by a power-by-wire flight-control system

A modern and updated flight simulator, which may be used for a greater fraction of pilot training to reduce the costly flight hours of the actual aircraft

Lightweight, powerful lithium-ion batteries to provide power to run the control surfaces in an emergency

Structural composites in the F-35 are 35% of the airframe weight (up from 25% in the F-22). The majority of these are bismaleimide and composite epoxy materials. The F-35 will be the first mass-produced aircraft to include structural nanocomposites, namely carbon nanotube-reinforced epoxy. Experience of the F-22's problems with corrosion led to the F-35 using a gap filler that causes less galvanic corrosion to the airframe's skin, designed with fewer gaps requiring filler and implementing better drainage. The relatively short 35-foot wingspan of the A and B variants is set by the F-35B's requirement to fit inside the Navy's current amphibious assault ship parking area and elevators; the F-35C's longer wing is considered to be more fuel efficient.

 

Costs

A U.S. Navy study found that the F-35 will cost 30 to 40% more to maintain than current jet fighters, not accounting for inflation over the F-35's operational lifetime. A Pentagon study concluded a $1 trillion maintenance cost for the entire fleet over its lifespan, not accounting for inflation. The F-35 program office found that as of January 2014, costs for the F-35 fleet over a 53-year lifecycle was $857 billion. Costs for the fighter have been dropping and accounted for the 22 percent life cycle drop since 2010. Lockheed stated that by 2019, pricing for the fifth-generation aircraft will be less than fourth-generation fighters. An F-35A in 2019 is expected to cost $85 million per unit complete with engines and full mission systems, inflation adjusted from $75 million in December 2013.

 

+++ DISCLAIMER +++

Nothing you see here is real, even though the model, the conversion or the presented background story might be based historical facts. BEWARE!

  

Some background:

The Georgian Air Force and Air Defense Division (თავდაცვის ძალების ავიაციისა და საჰაერო თავდაცვის სარდლობა; tavdatsvis dzalebis aviatsiisa da sahaero tavdatsvis sardloba) was established on January 1, 1992, and in September the Georgian Air Force conducted its first combat flight during the separatist war in Abkhazia. On August 18, 1998, the two divisions were unified in a joint command structure and renamed the Georgian Air Force.

In 2010, the Georgian Air Force was abolished as a separate branch and incorporated into the Georgian Land Forces as Air and Air Defense sections. By that time, the equipment – primarily consisting of Eastern Bloc aircraft inherited from the Soviet Union after the country’s dissolution – was totally outdated, the most potent aircraft were a dozen Suchoj Su-25 attack aircraft and a handful of MiG-21U trainers.

 

In order to rejuvenate the air arm, Tbilisi Aircraft Manufacturing (TAM), also known as JSC Tbilaviamsheni and formerly known as 31st aviation factory, started a modernization program for the Su-25, for the domestic forces but also for export customers. TAM had a long tradition of aircraft production within the Soviet Union. In the 1950s the factory started the production of Mikoyan's MiG-15 and later, the MiG-17 fighter aircraft. In 1957 Tbilisi Aircraft State Association built the MiG-21 two-seater fighter-trainer aircraft and its various derivative aircraft, continuing the MiG-21 production for about 25 years. At the same time the company was manufacturing the K-10 air-to-surface guided missile. Furthermore, the first Sukhoi Su-25 (known in the West as the "Frogfoot") close support aircraft took its maiden voyage from the runway of 31st aviation factory. Since then, more than 800 SU-25s had been delivered to customers worldwide. From the first SU-25 to the 1990s, JSC Tbilaviamsheni was the only manufacturer of this aircraft, and even after the fall of the Soviet Union the production lines were still intact and spares for more than fifty complete aircraft available. Along with the SU-25 aircraft 31st aviation factory also launched large-scale production of air-to-air R-60 and R-73 IR guided missiles, a production effort that built over 6,000 missiles a year and that lasted until the early 1990s. From 1996 to 1998 the factory also produced Su-25U two-seaters.

 

In 2001 the factory started, in partnership with Elbit Systems of Israel, upgrading basic Su-25 airframes to the Su-25KM “Scorpion” variant. This was just a technical update, however, intended for former Su-25 export customers who would upgrade their less potent Su-25K export aircraft with modern avionics. The prototype aircraft made its maiden flight on 18 April 2001 at Tbilisi in full Georgian Air Force markings. The aircraft used a standard Su-25 airframe, enhanced with advanced avionics including a glass cockpit, digital map generator, helmet-mounted display, computerized weapons system, complete mission pre-plan capability, and fully redundant backup modes. Performance enhancements included a highly accurate navigation system, pinpoint weapon delivery systems, all-weather and day/night performance, NATO compatibility, state-of-the art safety and survivability features, and advanced onboard debriefing capabilities complying with international requirements. The Su-25KM had the ability to use NATO-standard Mark 82 and Mark 83 laser-guided bombs and new air-to-air missiles, the short-range Vympel R-73. This upgrade extended service life of the Su-25 airframes for another decade.

There were, however, not many customers. Manufacturing was eventually stopped at the end of 2010, after Georgian air forces have been permanently dismissed and abolished. By that time, approximately 12 Scorpions had been produced, but the Georgian Air Force still used the basic models of Su-25 because of high cost of Su-25KM and because it was destined mainly for export. According to unofficial sources several Scorpions had been transferred to Turkmenistan as part of a trade deal.

 

In the meantime, another, more ambitious project took shape at Tbilisi Aircraft Manufacturing, too: With the help of Israel Aircraft Industries (IAI) the company started the development of a completely new attack aircraft, the TAM-1 “Gvelgeslas” (გველგესლას, Viper). It heavily relied on the year-long experience gathered with Su-25 production at Tblisi and on the tools at hand, but it was eventually a completely new aircraft – looking like a crossbreed between the Su-25 and the American A-10 with a T-tail.

 

This new layout had become necessary because the aircraft was to be powered by more modern, less noisy and more fuel-efficient Rolls Royce AE 3012 turbofan engines - which were originally intended to power the stillborn Yakovlev Yak-77 twin-engine business jet for up to 32 passengers, a slightly derated variant of the GMA 3012 with a 44 in diameter (112 cm) fan and procured via IAI from the United States through the company’s connection with Gulfstream Aerospace. Their larger diameter (the Su-25’s original Soyuz/Tumansky R-195 turbojets had a diameter of 109,5 cm/43.1 in) precluded the use of the former integral engine nacelles along the fuselage. To keep good ground clearance against FOD and to protect them from small arms fire, the engine layout was completely re-arranged. The fuselage was streamlined, and its internal structure was totally changed. The wings moved into a low position. The wings’ planform was almost identical to the Su-25’s, together with the characteristic tip-mounted “crocodile” air brakes. Just the leading edge inside of the “dogteeth” and the wing roots were re-designed, the latter because of the missing former engine nacelles. This resulted in a slightly increased net area, the original wingspan was retained. The bigger turbofans were then mounted in separate pods on short pylons along the rear fuselage, partly protected from below by the wings. Due to the jet efflux and the engines’ proximity to the stabilizers, these were re-located to the top of a deeper, reinforced fin for a T-tail arrangement.

 

Since the Su-25’s engine bays were now gone, the main landing gear had to be completely re-designed. Retracting them into the fuselage or into the relatively thin wings was not possible, TAM engineers settled upon a design that was very similar to the A-10: the aircraft received streamlined fairings, attached to the wings’ main spar, and positioned under the wings’ leading edges. The main legs were only semi-retractable; in flight, the wheels partly protruded from the fairings, but that hardly mattered from an aerodynamic point of view at the TAM-1’s subsonic operational speed. As a bonus they could still be used while retracted during emergency landings, improving the aircraft’s crash survivability.

 

Most flight and weapon avionics were procured from or via Elbit, including the Su-25KT’s modernized “glass cockpit”, and the TAM-1’s NATO compatibility was enhanced to appeal to a wider international export market. Beyond a total of eleven hardpoints under the wings and the fuselage for an external ordnance of up to 4.500 kg (9.900 lb), the TAM-1 was furthermore armed with an internal gun. Due to procurement issues, however, the Su-25’s original twin-barrel GSh-30-2 was replaced with an Oerlikon KDA 35mm cannon – a modern variant of the same cannon used in the German Gepard anti-aircraft tank, adapted to the use in an aircraft with a light-weight gun carriage. The KDA gun fired with a muzzle velocity of 1,440 m/s (4,700 ft/s) and a range of 5.500m, its rate of fire was typically 550 RPM. For the TAM-1, a unique feature from the SPAAG installation was adopted: the gun had two magazines, one with space for 200 rounds and another, smaller one for 50. The magazines could be filled with different types of ammunition, and the pilot was able select between them with a simple switch, adapting to the combat situation. Typical ammunition types were armor-piercing FAPDS rounds against hardened ground targets like tanks, and high explosive shells against soft ground targets and aircraft or helicopters, in a 3:1 ratio. Other ammunition types were available, too, and only 200 rounds were typically carried for balance reasons.

 

The TAM-1’s avionics included a SAGEM ULISS 81 INS, a Thomson-CSF VE-110 HUD, a TMV630 laser rangefinder in a modified nose and a TRT AHV 9 radio altimeter, with all avionics linked through a digital MIL-STD-1553B data bus and a modern “glass cockpit”. A HUD was standard, but an Elbit Systems DASH III HMD could be used by the pilot, too. The DASH GEN III was a wholly embedded design, closely integrated with the aircraft's weapon system, where the complete optical and position sensing coil package was built within the helmet (either the USAF standard HGU-55/P or the Israeli standard HGU-22/P), using a spherical visor to provide a collimated image to the pilot. A quick-disconnect wire powered the display and carried video drive signals to the helmet's Cathode Ray Tube (CRT).

 

The TAM-1’s development was long and protracted, though, primarily due to lack of resources and the fact that the Georgian air force was in an almost comatose state for several years, so that the potential prime customer for the TAM-1 was not officially available. However, the first TAM-1 prototype eventually made its maiden flight in September 2017. This was just in time, because the Georgian Air Force had formally been re-established in 2016, with plans for a major modernization and procurement program. Under the leadership of Georgian Minister of Defense Irakli Garibashvili the Air Force was re-prioritized and aircraft owned by the Georgian Air Force were being modernized and re-serviced after they were left abandoned for 4 years. This program lasted until 2020. In order to become more independent from foreign sources and support its domestic aircraft industry, the Georgian Air Force eventually ordered eight TAM-1s as Su-25K replacements, which would operate alongside a handful of modernized Su-25KMs from national stock. In the meantime, the new type also attained interest from abroad, e. g. from Bulgaria, the Congo and Cyprus. The IDF thoroughly tested two early production TAM-1s of the Georgian Air Force in 2018, too.

  

General characteristics:

Crew: 1

Length: 15.53 m (50 ft 11 in), including pitot

Wingspan: 14.36 m (47 ft 1 in)

Height: 4.8 m (15 ft 9 in)

Wing area: 35.2 m² (378 sq ft)

Empty weight: 9,800 kg (21,605 lb)

Gross weight: 14,440 kg (31,835 lb)

Max takeoff weight: 19,300 kg (42,549 lb)

 

Powerplant:

2× Rolls-Royce AE 3012 turbofans with 44.1 kN (9,920 lbf) thrust each

 

Performance:

Maximum speed: 975 km/h (606 mph, 526 kn, Mach 0.79)

Range: 1.000 km (620 mi, 540 nmi) with internal fuel, clean

Combat range: 750 km (470 mi, 400 nmi) at sea level with 4.500 kg (9,911 lb) of ordnance,

incl. two external fuel tanks

Service ceiling: 7.800 m (25,550 ft)

g limits: +6.5

Rate of climb: 58 m/s (11,400 ft/min)

 

Armament:

1× 35 mm (1.38 in) Oerlikon KDA cannon with 200 rds in two magazines

under the lower forward fuselage, offset to port side.

11× hardpoints with a capacity of up to 4.500 kg (9,911 lb) of external stores

  

The kit and its assembly:

This rather rigorous conversion had been on my project list for many years, and with the “Gunships” group build at whatifmodellers.com in late 2021 I eventually gathered my mojo to tackle it. The ingredients had already been procured long ago, but there are ideas that make you think twice before you take action…

 

This build was somewhat inspired by a CG rendition of a modified Su-25 that I came across while doing online search for potential ideas, running under the moniker “Su-125”, apparently created by someone called “Bispro” and published at DeviantArt in 2010; check this: (www.deviantart.com/bispro/art/Sukhoi-Su-125-Foghorn-15043...). The rendition shows a Su-25 with its engines re-located to the rear fuselage in separate nacelles, much like an A-10, plus a T-tail. However, as many photoshopped aircraft, the shown concept had IMHO some flaws. Where would a landing gear go, as the Su-125 still had shoulder wings? The engines’ position and size also looked fishy to me, quite small/narrow and very far high and back – I had doubts concerning the center of gravity. Nevertheless, I liked the idea, and the idea of an “A-10-esque remix” of the classic Frogfoot was born.

 

This idea was fueled even further when I found out that the Hobbycraft kit lends itself to such a conversion. The kit itself is not a brilliant Su-25 rendition, there are certainly better models of the aircraft in 1:72. However, what spoke for the kit as whiffing fodder was/is the fact that it is quite cheap (righteously so!) and AFAIK the only offering that comes with separate engine nacelles. These are attached to a completely independent central fuselage, and this avoids massive bodywork that would be necessary (if possible at all) with more conventional kits of this aircraft.

Another beneficial design feature is that the wing roots are an integral part of the original engine nacelles, forming their top side up to the fuselage spine. Through this, the original wingspan could be retained even without the nacelles, no wing extension would be necessary to retain the original proportions.

 

Work started with the central fuselage and the cockpit tub, which received a different (better) armored ejection seat and a pilot figure; the canopy remained unmodified and closed, because representing the model with an open cockpit would have required additional major body work on the spinal area behind the canopy. Inside, a new dashboard (from an Italeri BAe Hawk) was added, too – the original instrument panel is just a flat front bulkhead, there’s no space for the pilot to place the legs underneath the dashboard!

 

In parallel, the fin underwent major surgery. I initially considered an A-10-ish twin tail, but the Su-25’s high “tail stinger” prevented its implementation: the jet efflux would come very close to the tail surfaces. So, I went for something similar to the “Su-125” layout.

Mounting the OOB stabilizers to the fin was challenging, though. The fin lost its di-electric tip fairing, and it was cut into two sections, so that the tip would become long enough to match the stabilizers. A lucky find in the scrap box was a leftover tail tip from a Matchbox Blackburn Buccaneer, already shortened from a former, stillborn project: it had now the perfect length to take the Su-25 stabilizers! To make it fit on the fin, an 8mm deep section was inserted, in the form of a simple 1.5mm styrene sheet strip. Once dry, the surface was re-built with several PSR layers. Since it would sit further back on the new aircraft’s tail, the stinger with a RHAWS sensor was shortened.

 

On the fuselage, the attachment points for the wings and the engine nacelles were PSRed away and the front section filled with lots of lead beads, hoping that it would be enough to keep the model’s nose down.

 

Even though the wings had a proper span for a re-location into a low position, they still needed some attention: at the roots, there’s a ~1cm wide section without sweep (the area which would normally cover the original engine nacelles’ tops). This was mended through triangular 1.5 mm styrene wedges that extended the leading-edge sweep, roughly cut into shape once attached and later PSRed into the wings’ surfaces

 

The next construction site were the new landing gear attachment points. This had caused some serious headaches – where do you place and stow it? With new, low wings settled, the wings were the only logical place. But the wings were too thin to suitably take the retracted wheels, and, following the idea of a retrofitted existing design, I decided to adopt the A-10’s solution of nacelles into which the landing gear retracts forward, with the wheels still partly showing. This layout option appears quite plausible, since it would be a “graft-on” solution, and it also has the benefit of leaving lots of space for underwing stores, since the hardpoints’ position had to be modified now, too.

I was lucky to have a pair of A-10 landing gear nacelles at hand, left over from a wrecked Matchbox model from childhood time (the parts are probably 35 years old!). They were simply cut out, glued to the Su-25 wings and PSRed into shape. The result looked really good!

 

At this point I had to decide the model’s overall layout – where to place the wings, the tail and the new engine nacelles. The latter were not 1:72 A-10 transplants. I had some spare engine pods from the aforementioned Matchbox wreck, but these looked too rough and toylike for my taste. They were furthermore too bulky for the Su-25, which is markedly smaller than an A-10, so I had to look elsewhere. As a neat alternative for this project, I had already procured many moons ago a set of 1:144 resin PS-90A engines from a Russian company called “A.M.U.R. Reaver”, originally intended for a Tu-204 airliner or an Il-76 transport aircraft. These turbofan nacelles not only look very much like A-10 nacelles, just a bit smaller and more elegant, they are among the best resin aftermarket parts I have ever encountered: almost no flash, crisp molding, no bubbles, and perfect fit of the parts – WOW!

With these three elements at hand I was able to define the wings’ position, based on the tail, and from that the nacelles’ location, relative to the wings and the fin.

 

The next challenge: how to attach the new engines to the fuselage? The PS-90A engines came without pylons, so I had to improvise. I eventually found suitable pylons in the form of parts from F-14A underwing missile pylons, left over from an Italeri kit. Some major tailoring was necessary to find a proper position on the nacelles and on the fuselage, and PSRing these parts turned out to be quite difficult because of the tight and labyrinthine space.

 

When the engines were in place, work shifted towards the model’s underside. The landing gear was fully replaced. I initially wanted to retain the front wheel leg and the main wheels but found that the low wings would not allow a good ground clearance for underwing stores and re-arming the aircraft, a slightly taller solution was necessary. I eventually found a complete landing gear set in the scrap box, even though I am not certain to which aircraft it once belonged? I guess that the front wheel came from a Hasegawa RA-5C Vigilante, while the main gear and the wheels once belonged to an Italeri F-14A, alle struts were slightly shortened. The resulting stance is still a bit stalky, but an A-10 is also quite tall – this is just not so obvious because of the aircraft’s sheer size.

 

Due to the low wings and the landing gear pods, the Su-25’s hardpoints had to be re-arranged, and this eventually led to a layout very similar to the A-10. I gave the aircraft a pair of pylons inside of the pods, plus three hardpoints under the fuselage, even though all of these would only be used when slim ordnance was carried. I just fitted the outer pair. Outside of the landing gear fairings there would have been enough space for the Frogfoot’s original four outer for pylons, but I found this to be a little too much. So I gave it “just” three, with more space between them.

The respective ordnance is a mix for a CAS mission with dedicated and occasional targets. It consists of:

- Drop tanks under the inner wings (left over from a Bilek Su-17/22 kit)

- A pair of B-8M1 FFAR pods under the fuselage (from a vintage Mastercraft USSR weapon set)

- Two MERs with four 200 kg bombs each, mounted on the pylons outside of the landing gear (the odd MERs came from a Special Hobby IDF SMB-2 Super Mystère kit, the bombs are actually 1:100 USAF 750 lb bombs from a Tamiya F-105 Thunderchief in that scale)

- Four CBU-100 Rockeye Mk. II cluster bombs on the outer stations (from two Italeri USA/NATO weapon sets, each only offers a pair of these)

Yes, it’s a mix of Russian and NATO ordnance – but, like the real Georgian Su-25KM “Scorpion” upgrade, the TAM-1 would certainly be able to carry the same or even a wider mix, thanks to modified bomb racks and wirings. Esp. “dumb” weapons, which do not call for special targeting and guidance avionics, are qualified.

The gun under the nose was replaced with a piece from a hollow steel needle.

  

Painting and markings:

Nothing unusual here. I considered some more “exotic” options, but eventually settled for a “conservative” Soviet/Russian-style four-tone tactical camouflage, something that “normal” Su-25s would carry, too.

The disruptive pattern was adapted from a Macedonian Frogfoot but underwent some changes due to the T-tail and the engine nacelles. The basic tones were Humbrol 119 (RAF Light Earth), 150 (Forest Green), 195 (Chrome Oxide Green, RAL 6020) and 98 (Chocolate) on the upper surfaces and RLM78 from (Modelmaster #2087) from below, with a relatively low waterline, due to the low-set wings.

As usual, the model received a light black ink washing and some post-shading – especially on the hull and on the fin, where many details had either disappeared under PSR or were simply not there at all.

 

The landing gear and the lower areas of the cockpit were painted in light grey (Humbrol 64), while the upper cockpit sections were painted with bright turquoise (Modelmaster #2135). The wheel hubs were painted in bright green (Humbrol 101), while some di-electric fairings received a slightly less intense tone (Humbrol 2). A few of these flat fairings on the hull were furthermore created with green decal sheet material (from TL Modellbau) to avoid masking and corrections with paint.

 

The tactical markings became minimal, matching the look of late Georgian Su-25s. The roundels came from a Balkan Models Frogfoot sheet. The “07” was taken from a Blue Rider decal sheet, it actually belongs to a Lithuanian An-2. Some white stencils from generic MiG-21 and Mi-8 Begemot sheets were added, too, and some small markings were just painted onto the hull with yellow.

 

Some soot stains around the jet nozzles and the gun were added with graphite, and finally the kit was sealed with a coat of matt acrylic varnish.

  

A major bodywork project – and it’s weird that this is basically just a conversion of a stock kit and no kitbashing. A true Frogfoot remix! The new engines were the biggest “outsourced” addition, the A-10 landing gear fairings were a lucky find in the scrap box, and the rest is quite generic and could have looked differently. The result is impressive and balanced, though, the fictional TAM-1 looks quite plausible. The landing gear turned out to be a bit tall and stalky, though, making the aircraft look smaller on the ground than it actually is – but I left it that way.

From Wikipedia, the free encyclopedia

 

The Lockheed Martin F-35 "Lightning II" is a family of single-seat, single-engine, all-weather, stealth, fifth-generation, multirole combat aircraft, designed for ground-attack and air-superiority missions. It is built by Lockheed Martin and many subcontractors, including Northrop Grumman, Pratt & Whitney, and BAE Systems.

 

The F-35 has three main models: the conventional takeoff and landing F-35A (CTOL), the short take-off and vertical-landing F-35B (STOVL), and the catapult-assisted take-off but arrested recovery, carrier-based F-35C (CATOBAR). The F-35 descends from the Lockheed Martin X-35, the design that was awarded the Joint Strike Fighter (JSF) program over the competing Boeing X-32. The official Lightning II name has proven deeply unpopular and USAF pilots have nicknamed it Panther, instead.

 

The United States principally funds F-35 development, with additional funding from other NATO members and close U.S. allies, including the United Kingdom, Italy, Australia, Canada, Norway, Denmark, the Netherlands, and formerly Turkey. These funders generally receive subcontracts to manufacture components for the aircraft; for example, Turkey was the sole supplier of several F-35 parts until its removal from the program in July 2019. Several other countries have ordered, or are considering ordering, the aircraft.

 

As the largest and most expensive military program ever, the F-35 became the subject of much scrutiny and criticism in the U.S. and in other countries. In 2013 and 2014, critics argued that the plane was "plagued with design flaws", with many blaming the procurement process in which Lockheed was allowed "to design, test, and produce the F-35 all at the same time," instead of identifying and fixing "defects before firing up its production line". By 2014, the program was "$163 billion over budget [and] seven years behind schedule". Critics also contend that the program's high sunk costs and political momentum make it "too big to kill".

 

The F-35 first flew on 15 December 2006. In July 2015, the United States Marines declared its first squadron of F-35B fighters ready for deployment. However, the DOD-based durability testing indicated the service life of early-production F-35B aircraft is well under the expected 8,000 flight hours, and may be as low as 2,100 flight hours. Lot 9 and later aircraft include design changes but service life testing has yet to occur. The U.S. Air Force declared its first squadron of F-35As ready for deployment in August 2016. The U.S. Navy declared its first F-35Cs ready in February 2019. In 2018, the F-35 made its combat debut with the Israeli Air Force.

 

The U.S. stated plan is to buy 2,663 F-35s, which will provide the bulk of the crewed tactical airpower of the U.S. Air Force, Navy, and Marine Corps in coming decades. Deliveries of the F-35 for the U.S. military are scheduled until 2037 with a projected service life up to 2070.

 

Development

 

F-35 development started in 1992 with the origins of the Joint Strike Fighter (JSF) program and was to culminate in full production by 2018. The X-35 first flew on 24 October 2000 and the F-35A on 15 December 2006.

 

The F-35 was developed to replace most US fighter jets with the variants of a single design that would be common to all branches of the military. It was developed in co-operation with a number of foreign partners, and, unlike the F-22 Raptor, intended to be available for export. Three variants were designed: the F-35A (CTOL), the F-35B (STOVL), and the F-35C (CATOBAR). Despite being intended to share most of their parts to reduce costs and improve maintenance logistics, by 2017, the effective commonality was only 20%. The program received considerable criticism for cost overruns during development and for the total projected cost of the program over the lifetime of the jets.

 

By 2017, the program was expected to cost $406.5 billion over its lifetime (i.e. until 2070) for acquisition of the jets, and an additional $1.1 trillion for operations and maintenance. A number of design deficiencies were alleged, such as: carrying a small internal payload; performance inferior to the aircraft being replaced, particularly the F-16; lack of safety in relying on a single engine; and flaws such as the vulnerability of the fuel tank to fire and the propensity for transonic roll-off (wing drop). The possible obsolescence of stealth technology was also criticized.

  

Design

 

Overview

 

Although several experimental designs have been developed since the 1960s, such as the unsuccessful Rockwell XFV-12, the F-35B is to be the first operational supersonic STOVL stealth fighter. The single-engine F-35 resembles the larger twin-engined Lockheed Martin F-22 Raptor, drawing design elements from it. The exhaust duct design was inspired by the General Dynamics Model 200, proposed for a 1972 supersonic VTOL fighter requirement for the Sea Control Ship.

 

Lockheed Martin has suggested that the F-35 could replace the USAF's F-15C/D fighters in the air-superiority role and the F-15E Strike Eagle in the ground-attack role. It has also stated the F-35 is intended to have close- and long-range air-to-air capability second only to that of the F-22 Raptor, and that the F-35 has an advantage over the F-22 in basing flexibility and possesses "advanced sensors and information fusion".

 

Testifying before the House Appropriations Committee on 25 March 2009, acquisition deputy to the assistant secretary of the Air Force, Lt. Gen. Mark D. "Shack" Shackelford, stated that the F-35 is designed to be America's "premier surface-to-air missile killer, and is uniquely equipped for this mission with cutting-edge processing power, synthetic aperture radar integration techniques, and advanced target recognition".

 

Improvements

Ostensible improvements over past-generation fighter aircraft include:

 

Durable, low-maintenance stealth technology, using structural fiber mat instead of the high-maintenance coatings of legacy stealth platforms

Integrated avionics and sensor fusion that combine information from off- and on-board sensors to increase the pilot's situational awareness and improve target identification and weapon delivery, and to relay information quickly to other command and control (C2) nodes

High-speed data networking including IEEE 1394b and Fibre Channel (Fibre Channel is also used on Boeing's Super Hornet.

The Autonomic Logistics Global Sustainment, Autonomic Logistics Information System (ALIS), and Computerized maintenance management system to help ensure the aircraft can remain operational with minimal maintenance manpower The Pentagon has moved to open up the competitive bidding by other companies. This was after Lockheed Martin stated that instead of costing 20% less than the F-16 per flight hour, the F-35 would actually cost 12% more. Though the ALGS is intended to reduce maintenance costs, the company disagrees with including the cost of this system in the aircraft ownership calculations. The USMC has implemented a workaround for a cyber vulnerability in the system. The ALIS system currently requires a shipping-container load of servers to run, but Lockheed is working on a more portable version to support the Marines' expeditionary operations.

Electro-hydrostatic actuators run by a power-by-wire flight-control system

A modern and updated flight simulator, which may be used for a greater fraction of pilot training to reduce the costly flight hours of the actual aircraft

Lightweight, powerful lithium-ion batteries to provide power to run the control surfaces in an emergency

Structural composites in the F-35 are 35% of the airframe weight (up from 25% in the F-22). The majority of these are bismaleimide and composite epoxy materials. The F-35 will be the first mass-produced aircraft to include structural nanocomposites, namely carbon nanotube-reinforced epoxy. Experience of the F-22's problems with corrosion led to the F-35 using a gap filler that causes less galvanic corrosion to the airframe's skin, designed with fewer gaps requiring filler and implementing better drainage. The relatively short 35-foot wingspan of the A and B variants is set by the F-35B's requirement to fit inside the Navy's current amphibious assault ship parking area and elevators; the F-35C's longer wing is considered to be more fuel efficient.

 

Costs

A U.S. Navy study found that the F-35 will cost 30 to 40% more to maintain than current jet fighters, not accounting for inflation over the F-35's operational lifetime. A Pentagon study concluded a $1 trillion maintenance cost for the entire fleet over its lifespan, not accounting for inflation. The F-35 program office found that as of January 2014, costs for the F-35 fleet over a 53-year lifecycle was $857 billion. Costs for the fighter have been dropping and accounted for the 22 percent life cycle drop since 2010. Lockheed stated that by 2019, pricing for the fifth-generation aircraft will be less than fourth-generation fighters. An F-35A in 2019 is expected to cost $85 million per unit complete with engines and full mission systems, inflation adjusted from $75 million in December 2013.

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