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Fan trip for farewell of BR38 from Rottweil to Konstanz, here on the Einödtalbrücke near Tuttlingen, For this occasion the 038 382 carries its pre-computerized number

This was taken at the southwest corner of Broadway & 91st Street...

 

Note: this photo was published in a Jan 1, 2010 blog titled "Quad Band Dual SIM Cellphone – Slim Touchscreen Mobile (Black)." It was also published in a Jun 7, 2010 Technologeek blog, with the same title that I used as the caption on this Flickr page. And it was published in an Aug 16, 2010 Exotic Pet Information blog, with the same title that I used as the caption on this Flickr page. It was also published in a Dec 9, 2010 blog titled "What are the top ten best cellphones in the United States, besides the iPhone?"

 

Moving into 2011, the photo was published in an Apr 9, 2011 blog titled "Oktoberfest takes Cambridge’s portable stage."

 

***********************************

 

Looking back on some old photos from 40-50 years ago, I was struck by how visible the differences were between the culture of then, versus the culture of now. In some cases, it was evident from the things people wore, or carried, or did, back then which they no longer do today. But sometimes it was the opposite: things that didn't exist back in the 1960s and 1970s have become a pervasive part of today's culture.

 

A good example is the cellphone: 20 years ago, it simply didn't exist. Even ten years ago, it was a relatively uncommon sight, and usually only on major streets of big cities. Today, of course, cell phones are everywhere, and everyone is using them in a variety of culture contexts.

 

However, I don't think this is a permanent phenomenon; after all, if you think back to the early 1980s, you probably would have seen a lot of people carrying Sony Walkmans, or "boom-box" portable radios -- all of which have disappeared...

 

If Moore's Law (which basically says that computers double in power every 18 months) holds up for another decade, then we'll have computerized gadgets approximately 100 times smaller, faster, cheaper, and better -- which means far better integration of music, camera, messaging, and phone, but also the possibility of the devices being so tiny that they're embedded into our eyeglasses, our earrings, or a tattoo on our forehead.

 

So the point of this album is to provide a frame of reference -- so that we can (hopefully) look back 10-20 years from now, and say, "Wasn't it really weird that we behaved in such bizarre ways while we interacted with those primitive devices?"

via WordPress bit.ly/2gipQvb

Pernahkah Anda melihat Kencing Anda mengandung darah? Jika hal ini terjadi pada Anda, apakah yang harus Anda lakukan? Ketika saya pertama kali mengalaminya dulu, saya menjadi agak panik karena hal tersebut tidak pernah terjadi kepada saya.Jadi, pada artikel kali ini kita sama-sama akan mengetahui apakah yang seharusnya dilakukan jika urin mengandung darah.

 

sumber : bit.ly/2hcN5M1

 

Kehadiran darah di dalam air kencing dinamakan sebagai hematuria.Secara umumnya, hematuria ini ada 2 jenis.Jenis yang pertama adalah masalah di mana Anda tidak dapat melihat adanya darah di dalam kandungan air kencing dengan mata kasar.Ianya dapat terdeteksi hanya ketika dilihat menggunakan mikroskop. hematuria jenis ini disebut sebagai microscopic hematuria.

 

Jenis yang kedua adalah Anda dapat melihat dengan jelas urin Anda berwarna merah.Keadaan yang kedua ini dinamakan gross hematuria.Ini berarti yang Anda dapat melihat adanya darah di dalam air kemih hanya dengan melihat melalui mata telanjang.

 

Seringkali ketika terjadinya kondisi ini, persoalan yang sering muncul adalah “Apakah yang harus saya lakukan jika air kencing saya mengandung darah?” Atau “Haruskah saya khawatir kalau air kencing saya mengandung darah?” Mengapa hal ini membuat kita risau dan khawatir? Ini karena kebiasaannya kita tidak akan melihat darah ketika kita membuang air kecil.

 

Hematuria sebenarnya lebih ke tanda bagi masalah kesehatan anda dan ianya mendasari penyakit yang Anda hidapi.Perkara terbaik yang harus Anda lakukan adalah segeralah berkonsultasi dengan dokter jika Anda melihat darah di dalam air kencing.Ini penting karena dapat membantu menyembuhkan penyakit yang Anda hidapi.

 

Apakah penyebabnya?

 

Ada banyak sebab terjadinya hematuria.Sesetengahnya tidaklah begitu serius.Bagi beberapa orang, darah di dalam air kemih bisa hilang dengan sendirinya.Tetapi tidak ke beberapa individu yang lain di mana ia membutuhkan perawatan perubatan.Antara penyebab terjadinya hematuria kepada seseorang adalah:

 

Infeksi pada saluran kencing.Keadaan ini lebih banyak terjadi pada golongan wanita.Walau bagaimanapun juga dapat terjadi pada kaum lelaki.Jangkitan saluran kemih ini terjadi ketika mikroorganisme seperti bakteri memasuki saluran kemih Anda dan mereka akan berkembang biak di sana di mana ianya akan menyebabkan terjadinya peradangan pada saluran kencing dinamakan uretritis.Kadang-kadang bakteri ini akan menyebar ke organ-organ kemih lainnya seperti kandung kemih, ureter atau juga dapat menyebabkan infeksi pada ginjal.

 

Batu dalam ginjal atau kandung kencing.Beberapa zat di dalam urin Anda, terutama bila ia berkumpul, dapat membentuk batu kristal kecil. Kadang-kadang, batu kristal ini dapat menjadi lebih besar bila berada dalam jangka waktu yang lama di dalam ginjal atau kandung kemih anda.Batu yang terbentuk pada struktur saluran kemih yang lebih kecil dapat menyebabkan rasa sakit dan hematuria.

Kanker. Dalam beberapa kasus, adanya darah di dalam air kencing mungkin menjadi tanda bahwa terdapatnya sel kenser di dalam salah satu organ perkencingan anda.Namun, sebaiknya berkonsultasilah dengan dokter karena merekalah yang akan menentukan apakah hematuria Anda disebabkan oleh kanker atau tidak.

 

Obat-obatan. Beberapa obat dapat menyebabkan terjadinya hematuria terjadi, seperti aspirin, heparin dan antiobiotik tertentu.

Latihan. Kadang-kadang, hematuria juga bisa disebabkan dengan melakukan latihan yang berat.Ahli-ahli medis juga masih tidak mengetahui mengapa latihan dapat menyebabkan hematuria. Beberapa dari mereka percaya itu terjadi mungkin karena terjadi cedera pada kandung kemih.

Dalam beberapa kasus hematuria, penyebab yang sebenarnya tidak dapat ditemukan.

 

Diagnosa

 

Dokter Anda mungkin akan bertanya tentang masalah-masalah yang Anda hadapi dan akan melakukan pemeriksaan fisik secara menyeluruh. Kadang-kadang, mereka juga akan mengusulkan kepada Anda beberapa bentuk tes dan prosuder untuk menemukan penyebab masalah Anda dan juga untuk mengobati penyakit lain yang mungkin Anda hidapi. Contoh tes yang mungkin akan disarankan adalah menganalisis sampel air kencing dan juga tes pencitraan, seperti computerized tomography (CT) scan ataumagnetic resonance imaging (MRI), dan cystoscopy.

 

Perawatan

 

pengobatan yang dapat diambil untuk mengatasi masalah hematuria tergantung pada penyebabnya. Misalnya, jika hematuria disebabkan oleh infeksi pada saluran kemih, dokter akan memberikan obat antibiotik. Tetapi jika tidak ada masalah kesehatan yang serius ditemukan, mungkin tidak ada pengobatan yang khusus diperlukan.Walau bagaimanapun dokter mungkin masih akan menyarankan agar Anda melakukan perawatan tindak lanjut untuk memastikan masalah hematuria Anda sudah sembuh sepenuhnya.

+++ 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.

Details best viewed in Original Size

 

The Templo Expiatorio de la Sagrada Familia or Basilica and Expiatory Church of the Holy Family is a large unfinished Roman Catholic church in Barcelona, designed by Catalan architect Antoni Gaudí (1852–1926). Gaudí's work on the building is part of a UNESCO World Heritage Site, and in November 2010 Pope Benedict XVI consecrated and proclaimed it a minor basilica as distinct from a cathedral, which must be the seat of a bishop. In 1882, construction of Sagrada Família started under architect Francisco de Paula del Villar. In 1883, when Villar resigned, Gaudí took over as chief architect, transforming the project with his architectural and engineering style, combining Gothic and curvilinear Art Nouveau forms. Gaudí devoted the remainder of his life to the project, and at the time of his death at age 73 in 1926, less than a quarter of the project was complete. Relying solely on private donations, Sagrada Familia's construction progressed slowly and was interrupted by the Spanish Civil War, only to resume intermittent progress in the 1950s. Since commencing construction in 1882, advancements in technologies such as CAD (computer aided design) and CNC (Computerized Numerical Control) have enabled faster progress and construction passed the midpoint in 2010. However, some of the project's greatest challenges remain, including the construction of ten more spires, each symbolizing an important Biblical figure in the New Testament. It is anticipated that the building can be completed by 2026—the centenary of Gaudí's death. In which at first, he wished his city would be remembered for such an astonishing building.

In contrast to the highly decorated Nativity Façade, the Passion Façade is austere, plain and simple, with ample bare stone, and is carved with harsh straight lines to resemble the bones of a skeleton. Dedicated to the Passion of Christ, the suffering of Jesus during his crucifixion, the façade was intended to portray the sins of man. Construction began in 1954, following the drawings and instructions left by Gaudí for future architects and sculptors. The towers were completed in 1976, and in 1987 a team of sculptors, headed by Josep Maria Subirachs, began work sculpting the various scenes and details of the façade. They aimed to give a rigid, angular form to provoke a dramatic effect. Gaudí intended for this façade to strike fear into the onlooker. He wanted to "break" arcs and "cut" columns, and to use the effect of chiaroscuro (dark angular shadows contrasted by harsh rigid light) to further show the severity and brutality of Christ's sacrifice. Facing the setting sun, indicative and symbolic of the death of Christ, the Passion Façade is supported by six large and inclined columns, designed to resemble Sequoia trunks. Above there is a pyramidal pediment, made up of eighteen bone-shaped columns, which culminate in a large cross with a crown of thorns. Each of the four towers is dedicated to an apostle (James, Thomas, Philip, and Bartholomew) and, like the Nativity Façade, there are three porticos, each representing the theological virtues, though in a much different light.

Photoshop CS6 was used to clone out most construction cranes and other evidence that this is still an active construction site.

Additional information may be obtained at Wikipedia.

+++ 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.

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.

This was taken on the southwest corner of Broadway and 96th Street. I was concentrating on the woman in black, because I thought the combination of colors in her outfit was interesting. It was only after I uploaded the photograph, and cropped out the distracting elements in the picture, that I realized the significance of what I was left with ...

 

Note: this photo was published as an illustration in a Jul 2009 Squidoo blog titled "Buying Cell Phones on Ebay." It was also published in an undated (September 2009) blog titled "We're all Gadget Geeks Now!." And it was published as an illustration in an Oct 2009 Squidoo blog titled "Samsung Omnia Review." It was also published in a Nov 5, 2009 Atlantic Monthly blog titled "What's Wrong With Your Cell Phone Company." And it was published in a Nov 25, 2009 blog titled "Tips for Buying Cell Phone."

 

Moving into 2010, the photo was published in a May 28, 2010 Technologeek blog, with the same title as the caption that I used on this Flickr page. And it was published in a Jun 4,2010 Popwuping(?) blog titled "Cell Phone Culture."

 

Moving into 2011, the photo was published in a Jan 30, 2011 blog titled "Cell Phone Look Up Directory – How To Trace a Cell Phone Number Comfortably From Home." It was also published in a May 31, 2011 blog titled "So Your Cell Phone Causes Cancer ... Now What?"

 

Moving into 2012, the photo was published in a Mar 7, 2012 blog titled "PayPal México ve el futuro en los cellars." It was also published in a Jul 16, 2012 blog titled "Research: smartphone and tablet users act on clicked ads." And it was published in an Aug 3, 2012 blog titled "1152 個美國人邊走邊玩手機,最後也走進了急診室." It was also published in an Aug 24, 2012 blog titled "'Wall Street Journal' Offers Free Wi-Fi in NYC, San Francisco.." And it was published in an Oct 17, 2012 blog titled "One Nation, Under Surveillance." Also, a severely cropped version of the photo was published in a Nov 13, 2012 blog titled "Oslo-polisen frestar ficktjuvar med falsk Iphone 5."

 

More recently, I found that the photo was published in an Aug 11, 2012 blog titled "Er det ikke best å utvikle apps til iOS først?"

 

Moving into 2013, the photo was published in a Jan 11, 2013 blog titled "Slow Thinking in a Fast World." And it was published in an undated (mid-Feb 2013) blog titled "How Long Should Your Phone Number Be?" And it was published in a Feb 15, 2013 blog titled "Stay local! magazine." It was also published in a Mar 2, 2013 blog titled "Can the Human Race Survive the Negative Side of Social Media?" And it was published in a Mar 19, 2013 blog titled "Could Your Smartphone Be Hacked?" It was also published in a Mar 31, 2013 blog titled "Baterías, la asignatura pendiente de los dispositivos electrónicos." A tightly cropped version of the photo was also published in a May 1, 2013 blog titled "#21 PITTSBURGH CITY ALERT: A MOBILE APP TO KEEP YOU CONNECTED." And the photo was published in a May 8, 2013 blog titled "What Phone Companies Are Doing With All That Data From Your Phone" It was, as well as a May 25, 2013 blog similarly titled "Smithsonian: What Phone Companies Are Doing With All That Data From Your Phone." It was also published in a May 16, 2013 blog titled "IDC: Android OEMs Shipped 162M Smartphones In Q1, More Than 4X Apple’s Rate; Windows Phone Now In (Distant) Third." And it was published in a Jun 21, 2013 blog titled "When Big Data Really Means Small Data." It was also published in a Jul 3, 2013 blog titled "Mobile Data Traffic To Grow 300% Globally By 2017 Led By Video, Web Use, Says Strategy Analytics," as well as a Jul 25, 2013 blog titled "ADICTOS A LAS NUEVAS TECNOLOGÍAS." It was also published in an Aug 16, 2013 blog titled "Student Housing: What’s really important to today’s college renter."

 

Moving into 2014, the photo was published in a Mar 11, 2014 Washington Post blog titled These 2,500 experts predicted the future of the Web. It looks a lot like the present." It was also published in a Jun 18, 2014 Washington Post article titled "The ACLU’s latest lawsuit on warrantless cellphone tracking has hit a dead end." And it was published in an Aug 30, 2014 blog titled "How Technology is Compromising the Human Condition."

 

*****************************************

 

Looking back on some old photos from 40-50 years ago, I was struck by how visible the differences were between the culture of then, versus the culture of now. In some cases, it was evident from the things people wore, or carried, or did, back then which they no longer do today. But sometimes it was the opposite: things that didn't exist back in the 1960s and 1970s have become a pervasive part of today's culture.

 

A good example is the cellphone: 20 years ago, it simply didn't exist. Even ten years ago, it was a relatively uncommon sight, and was seen usually only on major streets of big cities. Today, of course, cell phones are everywhere, and everyone is using them in a variety of cultural contexts.

 

However, I don't think this is a permanent phenomenon; after all, if you think back to the early 1980s, you probably would have seen a lot of people carrying Sony Walkmans, or "boom-box" portable radios -- all of which have disappeared...

 

If Moore's Law (which basically says that computers double in power every 18 months) holds up for another decade, then we'll have computerized gadgets approximately 100 times smaller, faster, cheaper, and better -- which means far better integration of music, camera, messaging, and phone, but also the possibility of the devices being so tiny that they're embedded into our eyeglasses, our earrings, or a tattoo on our forehead.

 

So the point of this album is to provide a frame of reference -- so that we can (hopefully) look back 10-20 years from now, and say, "Wasn't it really weird that we behaved in such bizarre ways while we interacted with those primitive devices?"

Graymont's Pilot Peak plant is one of the most modern and efficient lime plants in North America. The stone is quarried immediately adjacent to the plant, crushed to size and conveyed directly to the preheater kilns.

 

The raw material is processed in a modern, fully computerized plant which is controlled by the latest quality assurance technologies. These technologies allow us to provide our customers with a reliable supply of the highest quality lime available. A full range of sized bulk quicklime products is available. The plant is equipped with a hydrator capable of producing 300 tons of hydrated lime per day. Storage and shipping facilities are available for truck and rail delivery to customers.

 

www.graymont.com/en/locations/lime-plants/western-us/lime...

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.

Student pilots in the Air Force’s first Lockheed Martin F-35A Lightning II "Joint Strike Fighter" basic flight course class took to the skies for the first time as they entered the live flying portion of their training Feb. 8, 2017 at Luke Air Force Base. The B-course (basic flight course class) students, training under the tutelage of the experienced instructor pilots of the 61st Fighter Squadron, will become the first purely operational combat F-35 pilots in the Air Force.

 

Lockheed Martin F-35A Lightning II "Joint Strike Fighter" (sn 11-5044 (MSN AF-55) and Lockheed Martin F-35A Lightning II "Joint Strike Fighter" (sn 11-5041) (MSN AF-52)

  

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.

Well I'm starting to decide to jump in like so many others and try to supplement my income via photography. My primary career is and has been a remodeling and building business the past decade and now I've reached the age of 50... working on high ladders, steep roofs and on the knees all day tiling a floor no longer has the same appeal. Can still hang in there rather well, but for the first time in my life it's starting to "feel" more difficult than previous as I would always tell others around me there isn't anything to it...easy work. Combine that with an economy that has been stuck in the ditch for years with little sign or hope of improvement, owners are not willing to invest in their homes when the money spent on upgrades will simply vanish...and people now generally a first class pain in negotiations. Financing for most is impossible and materials are outrageously high. I wonder if it will ever recover in my area.

 

I'll still be doing it for the short term but at the age where I need to do something else. I find it important to do something enjoyable as I've had jobs I hated when younger and will never go back. I've seen better artists than I struggle in photography endeavors, but diversifying into 2 half paced markets will add up to one. I have never made any effort to get my stuff out there other than Flickr, so now hope to soon add a website and become "visible". Right now the name I have chosen would be "Landscapes of the Blue Ridge" since I'm not too fond of "insert name photography".

 

I have previously done framing, matting and completed pictures, and my father-in-law has a state of the art frame shop with computerized matting device, he knows lots of great methods of making things top quality so that should be a big help. Not looking to be in a big hurry as spring is really my busy time in construction, just plod along and hope I can make it work.

'Close-Up' from 'Recorders' by Raphael Lozano-Hemmer.

 

"Close-up" is an interactive display with a built-in computerized tracking system. This piece shows the viewer's shadow revealing hundreds of tiny videos of other people who have recently looked at the work. When a viewer approaches the piece, the system automatically starts recording and makes a video of him or her. Simultaneously, inside the viewer's silhouette videos are triggered that show up to 800 recent recordings. This piece presents a schizoid experience where our presence triggers a massive array of surveillance videos.

 

Manchester, UK.

 

28 October, 2010.

 

My Recorders set.

 

Check out Rob of Rochdale's wonderful take on this same piece. :-)

My first Bench Monday. I've given in to the craze. I figure it could be fun, and if nothing else it will give me a theme for my Mondays.

 

Holy geez, I couldn't figure out what number today was! I can't just look at the calendar and figure it out anymore. Gah!

 

Feb. 1

 

amybean365.blogspot.com

Judges observe as a weapons load crew from the 62nd Aircraft Maintenance Unit prepares an inert bomb for loading on a Lockheed Martin F-35A Lightning II "Joint Strike Fighter" during the 2018 1st Quarter Load Crew Competition at Luke Air Force Base, Ariz., April 6. The 62nd AMU team beat five other teams to win the competition.

  

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.

Another attempt at Andromeda, this time with my 400 mm and a tracking mount! (Using a dovetail adapter on a 4SE computerized mount, nothing fancy.) I stacked about 55 exposures, using 13 seconds, f/2.8, ISO 3200 per exposure. Total integration time is around 11.5 minutes. Wasn't the best viewing conditions, and combined with [alt/az] tracking errors, wind, and possibly slightly inaccurate focus, has resulted in slightly blobby stars. Still pleased with this image, and looking forward to next attempt!

A well used car

 

The Chevrolet Celebrity is an automobile that was produced by the Chevrolet division of General Motors. Sold from the 1982 to 1990 model years, a single generation of the Celebrity was produced, replacing the Malibu as the mid-size Chevrolet model range. During the early 1960s, the nameplate was first used by Oldsmobile for the pillared sedan version of the Oldsmobile 88.

 

It is based on the front-wheel drive GM A platform, and was produced alongside the Buick Century, Oldsmobile Cutlass Ciera, and Pontiac 6000. The interior space and running gear are the same as the compact Citation, but Celebrity is trimmed and equipped better. Power steering/brakes and automatic transmission were standard in 1982-83; automatic optional later. Most used cars have all three. A roomy 5-door wagon debuted for 1984 and so did a Eurosport handling/ appearance package. The base 2.5-liter four lacks power to haul a full load. A high-output fuel-injected V-6 became optional for '85, but the carbureted version had fewer driveability woes. Diesel power departed after '85. Generation II engines, reworked for 1987, have fuel injection, and a new Getrag-designed 5-speed manual shift became available with the V-6. Balance shafts were added to the Tech IV engine for '88. The 4-cylinder engine gained 12 horsepower late in the 1989 model year. Two-doors sold poorly and were dropped for '89.

 

Celebrity is more spacious than a bigger Malibu, with front-wheel-drive traction and responsive handling. However, gas mileage isn't better. Workmanship has been good, so these cars have bettered the dismal recall record of their X-car parents. There have been some driveability problems with the computerized engine control system in 1982 models, and deterioration of the upper engine-torque strap causes engine/transaxle vibration. Only the station wagon remained for the 1990 model year, with a new optional 3.1 liter V-6 engine.

 

For the 1990 model year, the Celebrity sedan was discontinued, replaced by the Chevrolet Lumina, with the Chevrolet Lumina APV minivan replacing the station wagon, which ended production after the 1990 model year.

61st Aircraft Maintenance Unit maintainers inspects an Lockheed Martin F-35A Lightning II "Joint Strike Fighter" (sn 11-5037) (MSN AF-48) prior to its taxi-out and takeoff July 18, 2018, at Luke Air Force Base, Ariz. Pilots and maintainers perform thorough pre-flight checks before each sortie.

  

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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In 1974, a construction worker, George Hanson, unearthed unusual bones while the area was being prepared for a new subdivision. His son recognized one of the finds as a mammoth tooth.

The landowner Phil Anderson agreed to further investigation, and a complete skull and tusk were found in 1974. Phil Anderson agreed to donate the entire bone bed and mineral rights to the nonprofit organization and along with the work performed by amateur and professional excavators, led to its status as a museum, and it was designated a National Natural Landmark in 1980. Initially the finds were mapped on a string grid; since then the mapping systems have increasingly relied on computerized technologies.

The Mammoth Site of Hot Springs, SD is an active paleontological dig site, which boasts the largest concentration of mammoth remains in the world! Our current mammoth count is 61, with 58 Columbian and 3 woolly mammoths. We hope you will come and tour this unique National Natural Landmark!

Paleontology is the study of pre-existing life based on fossils. A fossil could be an actual portion of the animal, such as bones, teeth, or shells, or maybe replaced by minerals such as silica, iron and manganese as in petrified wood. A fossil may also be a track or a trail, an imprint or a cast, anything that indicates preexisting life forms. Through paleontology, scientists hope to create a more complete understanding of how life has changed since it first appeared in the geologic record of time.

The majority of fossils found at the Mammoth Site are from the North American Columbian mammoth. Evidence of three woolly mammoths have also been discovered here, making this “east meets west mammoth gathering” the first time both species have been found together. Fossils of other Ice Age animals have also been discovered: camel, llama, giant short-faced bear, wolf, coyote and prairie dog to name a few. Imprint fossils of bird feathers, complete fish skeletons, and thousands of mollusk shells have also been recovered from this now-dry 26,000 year old sinkhole.

Not petrified, these fossils are dry and fragile. The bones, scat and shells are identified, numbered cataloged and preserved, with almost all the mammoth remains displayed in-situ (as they were found in the sinkhole).

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I watched this woman sitting alone, at the 72nd Street entrance on the west Side of Central Park, looking very unhappy; she clutched her cellphone in her hands but didn't use it, as if she was waiting for a call. After about 5-10 minutes, a guy came along and greeted her; click here to see him. I assume he was the boyfriend, but in any case, she continued clutching her cellphone...

 

Note: this photo was published in a Jun 12, 2009 blog titled "Unhappy? Stop trying to be happier." And a cropped version of the photo was published in a Sep 23, 2009 German blog titled "Wie lange auf den Anruf warten?" It was also published in a Jul 4, 2010 blog titled "Is Your Income Standard Too Low?" And it was also published in an Oct 5, 2011 blog titled Tolle Computerized Bilder, with the same caption and detailed notes that I had written on this Flickr page.

 

Moving into 2012, the photo was published in an Apr 24, 2012 blog titled "4 Ways to Stay Sane in a Toxic Office."

 

****************************

 

Looking back on some old photos from 40-50 years ago, I was struck by how visible the differences were between the culture of then, versus the culture of now. In some cases, it was evident from the things people wore, or carried, or did, back then which they no longer do today. But sometimes it was the opposite: things that didn't exist back in the 1960s and 1970s have become a pervasive part of today's culture.

 

A good example is the cellphone: 20 years ago, it simply didn't exist. Even ten years ago, it was a relatively uncommon sight, and usually only on major streets of big cities. Today, of course, cell phones are everywhere, and everyone is using them in a variety of culture contexts.

 

However, I don't think this is a permanent phenomenon; after all, if you think back to the early 1980s, you probably would have seen a lot of people carrying Sony Walkmans, or "boom-box" portable radios -- all of which have disappeared...

 

If Moore's Law (which basically says that computers double in power every 18 months) holds up for another decade, then we'll have computerized gadgets approximately 100 times smaller, faster, cheaper, and better -- which means far better integration of music, camera, messaging, and phone, but also the possibility of the devices being so tiny that they're embedded into our eyeglasses, our earrings, or a tattoo on our forehead.

 

So the point of this album is to provide a frame of reference -- so that we can (hopefully) look back 10-20 years from now, and say, "Wasn't it really weird that we behaved in such bizarre ways while we interacted with those primitive devices?"

Another attempt at the HST palette.......a little closer

Red=OIII

Green=Ha

Blue=OIII

 

Orion ED102T CF Triplet Apochromatic Refractor Telescope.-RGB & OIII

Orion ST-80T "guide scope"-Ha

Orion Sirius German-equatorial Computerized Goto Mount

Images aquired using APT

Guided with Starshoot Autoguider and 50mm guide scope

Aligned and stacked with Nebulosity

Post-process with StarTools GIMP & Windows Live Photo

 

32 total frames: (3hrs 40 min) using an equal # of dark frames

OIII-4x300 5x600 iso 800 Canon T3i with Astronomik OIII clip-in filter

Ha-4x300 5x600 3x900 iso 800 Canon T3(modified) with Astronomik Ha clip-in filter

RGB- 6x300 5x600 iso 800 Canon T3i no filters

 

sites.google.com/site/astrochuck123

 

*****Check out my "terrestrial" pictures on:

www.flickr.com/photos/78400750@N07

 

This was taken at the southwest corner of Broadway and 92nd Street; behind the woman is a PetCo pet-supply company.

 

Note: this photo was published in a Feb 17, 2010 Hot Mobile Phone offers blog with the same title as the caption I used on this Flickr page. It was also published in an Apr 20, 2010 LifeHacker blog, with the title"Organize Your Work Contacts by Company on Your Phone with a Simple Tweak." And it was published in a May 30, 2010 Technologeek blog, with the same title as the caption that I used on this Flickr page. It was also published in an undated (Jun 2010) Cheap Tattoo blog, with the same title as the caption that I used on this Flickr page. It was also published in an Aug 19, 2010 blog titled "Technology Abuse." And it was published in a Sep 1, 2010 blog titled "A Woman’s Perspective on Personal Self Defense."

 

Moving into 2011, the photo was published in a Mar 10, 2011 blog titled "Text Messaging with Google Voice? The Right Setting Depends Upon Your Particular Phone." And it was published in an Apr 9, 2011 blog titled "Las cuatro alternativas más usadas para enviar mensajes gratis a móviles." It was also published in a May 25, 2011 Getting a Tattoo Ideas, with the same caption and detailed notes that I had written on this Flickr page. And it was published in an Aug 30, 2011 Martial Arts Lovers blog, with the same caption that I used on this Flickr page.

 

Moving into 2012, the photo was published in a Jan 15, 2012 blog titled "I HAVE SOME A PROBLEM FOR TATTOO MACHINE AND POWER SUPPLY?" It was also published in a Jul 24, 2012 blog titled "Vocablet of the day: oblivion." And it was published in an Aug 8, 2012 blog titled "EASY WAYS TO MAKE DROP-OFF GREAT ON THE FIRST DAY OF PRESCHOOL."

 

Moving into 2013, the photo was published in a Mar 4, 2013 blog titled "Pulling Back The Curtain On Text Message Mobile Marketing." And it was published in a May 5, 2013 blog titled "Used Cellphones - Cheap Phones."

 

Moving into 2014, the photo was published in a Jan 6, 2014 blog titled "Different Ways Women Can Use Instant Messengers."

 

******************

Note: on Apr 20, 2010 I decided to make a couple minor editing changes. The primary objective was to reduce the extent of dark shadow (i.e., solid black color) in the woman's pants and jacket, so that you would be able to see some shades of color. There was also a bit of over-exposure ("hot spot") on the top left portion of her t-shirt...

******************

 

Looking back on some old photos from 40-50 years ago, I was struck by how visible the differences were between the culture of then, versus the culture of now. In some cases, it was evident from the things people wore, or carried, or did, back then which they no longer do today. But sometimes it was the opposite: things that didn't exist back in the 1960s and 1970s have become a pervasive part of today's culture.

 

A good example is the cellphone: 20 years ago, it simply didn't exist. Even ten years ago, it was a relatively uncommon sight, and was seen usually only on major streets of big cities. Today, of course, cell phones are everywhere, and everyone is using them in a variety of cultural contexts.

 

However, I don't think this is a permanent phenomenon; after all, if you think back to the early 1980s, you probably would have seen a lot of people carrying Sony Walkmans, or "boom-box" portable radios -- all of which have disappeared...

 

If Moore's Law (which basically says that computers double in power every 18 months) holds up for another decade, then we'll have computerized gadgets approximately 100 times smaller, faster, cheaper, and better -- which means far better integration of music, camera, messaging, and phone, but also the possibility of the devices being so tiny that they're embedded into our eyeglasses, our earrings, or a tattoo on our forehead.

 

So the point of this album is to provide a frame of reference -- so that we can (hopefully) look back 10-20 years from now, and say, "Wasn't it really weird that we behaved in such bizarre ways while we interacted with those primitive devices?"

LEMOORE, California (June 5, 2019) The first Marine Fighter Attack Squadron (VMFA) 314 "Black Knights" Lockheed Martin F-35C Lightning II aircraft from Naval Air Station (NAS) Lemoore flown by CAPT Tommy Beau Locke from Strike Fighter Squadron (VFA) 125 "Rough Raiders" flies in formation over the Sierra's with the VFMA-314 squadron F/A-18A++, flown by LtCol Cedar Hinton aircraft "passing the lead" as part of the F/A-18 Sundown with the Black Knights.

  

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.

LEMOORE, California (June 5, 2019) The first Marine Fighter Attack Squadron (VMFA) 314 "Black Knights" Lockheed Martin F-35C Lightning II aircraft from Naval Air Station (NAS) Lemoore flown by CAPT Tommy Beau Locke from Strike Fighter Squadron (VFA) 125 "Rough Raiders" flies in formation over the Sierra's with the VFMA-314 squadron F/A-18A++, flown by LtCol Cedar Hinton aircraft "passing the lead" as part of the F/A-18 Sundown with the Black Knights.

  

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.

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 4844-1).

 

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

I was gifted the T70 by a friend, along with 28 mm wide-angle and 70-210 zoom lenses, after he went digital and no longer wanted anything to do with film.

As Ken Rockwell’s review of this camera states “the T70, along with the T50, began the computerized camera era for Canon. The T70 is among Canon's last manual-focus cameras”. It uses Canon's manual-focus FD lenses so there is no compatibility with Canon’s autofocus, EOS film or EOS digital cameras. This one has the f1.8 50 mm although an f1.4 was an option. Lens quality was never a problem.

As such this gimmicky approach by Canon never appealed to me. I preferred the manual solution (at least as far as film cameras were concerned). To my mind there was and is something inherently more trustworthy about a film-transport and shutter-cocking system that relied upon a small thumb-powered lever or add-on motor drive/winder. But then I would never willingly drive an automatic car, the term Luddite might occur to some readers.

Having said that, the T70 does what it does very well and has much to commend it:

Multiple Program AE (Three modes Standard/Wide/Tele)

Two metering modes (Partial and Averaging)

Uses the ubiquitous AA battery (inc. rechargeable ones)

Large bright viewfinder (superior to many modern digital SLRs)

More comfortable in the hands than either the AE-1 or A1

There are limitations too:

Shutter Priority only (no Aperture Priority)

Manual mode only controlled by faffing about with buttons

No AEL

No conventional cable release facility

No DoF preview (really?)

It was the last two of these that, to me, damned this camera as a glorified point & shoot in SLR form, however, it fits one of the main criteria for my collection because it is an interesting development in camera design.

 

See more photos of this, and the Wikipedia article.

 

Details, quoting from 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.

 

Long Description:

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.

Decided to re-image the Swan Nebula. Last years result is in the comments section.( You may have to squint to see the Swan!)

 

Orion ED102T CF Triplet Apochromatic Refractor Telescope.

Orion Sirius German-equatorial Computerized Goto Mount

 

Images aquired using APT

Guided with Starshoot Autoguider and 50mm guide scope

Aligned and stacked with Nebulosity

Post-process with StarTools GIMP & Windows Live Photo

 

21 total frames: (2hrs 25min)

8x600 iso 800 Canon T3(modified) with Astronomik Ha clip-in filter w/Orion ST-80T

13x300 iso 800 Canon T3i no filters w/Orion ED 102mm

 

sites.google.com/site/astrochuck123

 

*****Check out my "terrestrial" pictures on:

www.flickr.com/photos/78400750@N07/

 

Within the 2-degree view in the eyepiece were three Open Clusters (NGC 2335, NGC 2342 & Collinder 466) and one Asterism (Collinder 466); all dwarfed by the ethereal background glow of the northern extension of the Seagull Nebula (IC 2177). As the jigsaw puzzle of celestial marvels flooded my eye, I at first, ignored the pencil and paper at my side, and just focused at the complex star field. How could I ever dream of capturing this to paper? The answer of course, is that I never could, but that was not the point. The objective was to produce something that would remind me days, months, years later of what I was seeing tonight. I knew that just the act of drawing would make me see detail that otherwise would go unnoticed. Relax, enjoy the view, then start sketching and taking notes – take it one step at a time – don’t rush -- the rest of the world and all the other objects in the night sky can wait for another time.

 

As has happened so my times before, a lot of telescope time passed unnoticed. At the end I had several small-detailed rough drawings at 182x and a large-overall rough drawing at 52x; a couple of sketches were done with nebula filters but most without.

 

The above final computerized drawing is a composite of all the rough sketches/notes mixed with my overall visual impression of a very tiny, tiny section of the night sky, deep in the constellation of the Unicorn, as it appeared to me, and me alone, on February 14, 2020.

 

To see additional astronomy drawings visit: www.orrastrodrawing.com

 

We arrived at the Peak Tram lower terminal. We had bought "priority entrance" tickets when we exited MRT Central Station. Yeh, right. About 45 minutes later we were squeezed onto the tram. Unbelievably busy and this was early morning.

 

The system was comprehensively rebuilt in 1989 by Swiss company, Von Roll, with a new track, a computerized control system, and two new two-car trams with a capacity of 120 passengers per tram.

 

By 1997, the system carried some 2 million passengers annually. Today, more than 4 million people ride the Peak Tram annually, or an average of over 11,000 every day. OMG!

 

The tram first began operating 30 May, 1888. The tram passes six stations along its 4,478 feet length at a slope of 27 degrees and takes 7 minutes to reach the top.

Lake Express is the first high speed auto/passenger ferry to operate on a route on both the Great Lakes and within the Continental United States. The aluminum hulled catamaran was built at Austal USA, LLC's aluminum shipbuilding facility in Mobile, Alabama and was launched on March 20, 2004. The ship began service on the route between Milwaukee, Wisconsin and Muskegon, Michigan on June 1, 2004.

 

Lake Express...

 

* Reaches speeds of up to 34 knots (40mph).

* Is equipped with a self actuating computerized ride control system, providing a smoother ride and fewer cancellations due to lake conditions.

* Uses state-of-the-art radar, fire suppressant systems, Global Positioning Systems and engine room monitoring systems.

* Is powered by four diesel engines producing 3000hp each which drive four independent water jets.

 

Source: www.lake-express.com

 

This woman was walking up Broadway, at 81st Street. I think I could have walked right into her, and knocked her flat on the ground, before she would have noticed me...

 

**********************************************************

 

Note: this photo was published in a Jun 23, 2010 "Technologeek blog, with the same title as the caption I used on this Flickr page. And it was published in an Aug 26, 2010 blog titled "What's So Wrong With Facebook Places?", as well as an Aug 26, 2010 blog titled "Three mobile web marketing tips for the holiday shopping season."

 

Moving on to 2011, the photo was published in a Feb 15, 2011 blog titled "Get Your Retail Therapy On In Villa Rica!" And it was published in a Feb 20, 2011 Cool Web Tips Marketing Images blog, with the same caption and detailed notes that I had written on this Flickr page. It was also published in an undated (early Mar 2011) vi.sualize.us blog. And it was published in a Jun 24, 2011 blog titled "UK mobile networks team up on handset payments system." It was also published in a Jul 5, 2011 MobileBeat blog titled "Juniper: Mobile Payments to hit 0 billion by 2015," as well as a Jul 5, 2011 blog titled Top 10 Best Business Ipad Apps For Sales micklehurstallsaintschurch.org/top-10-best-business-ipad-...

 

Moving into 2012, the photo was published in a Jan 1, 2012 blog titled "Mobile Apps for the Holidays." And it was published in an undated (mid-Jun 2012) blog titled "M-commerce: Now is the time for action!." It was also published in a Jul 17, 2012 blog titled "Get Off Your Cellphone And 9 Other Tips For Not Getting Mugged." And it was published in a Jul 26, 2012 blog titled "Growth of Mobile Commerce," as well as a Jul 26, 2012 Business Insider blog titled " Former Headhunter Explains How To Answer 11 Tough Interview Questions." It was also published in a Nov 15, 2012 blog titled "Report: mobile payments to hit $1 trillion by 2017." And it was published in a Dec 7, 2012 blog titled "MOBILE SHOPPING, A RETAIL OPPORTUNITY."

 

Moving into 2013, the photo was published in a Mar 22, 2013 blog titled "Millennials Marketing: Mobile & Social Media Required." It was also published in an Oct 16, 2013 blog titled "Women: Reduce Your Chances of Assault."

 

Moving into 2014, the photo was published in a Sep 17, 2014 blog titled "Las chicas andan por la calle mirando a sus móviles más que los chicos."

 

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Looking back on some old photos from 40-50 years ago, I was struck by how visible the differences were between the culture of then, versus the culture of now. In some cases, it was evident from the things people wore, or carried, or did, back then which they no longer do today. But sometimes it was the opposite: things that didn't exist back in the 1960s and 1970s have become a pervasive part of today's culture.

 

A good example is the cellphone: 20 years ago, it simply didn't exist. Even ten years ago, it was a relatively uncommon sight, and usually only on major streets of big cities. Today, of course, cell phones are everywhere, and everyone is using them in a variety of culture contexts.

 

However, I don't think this is a permanent phenomenon; after all, if you think back to the early 1980s, you probably would have seen a lot of people carrying Sony Walkmans, or "boom-box" portable radios -- all of which have disappeared...

 

If Moore's Law (which basically says that computers double in power every 18 months) holds up for another decade, then we'll have computerized gadgets approximately 100 times smaller, faster, cheaper, and better -- which means far better integration of music, camera, messaging, and phone, but also the possibility of the devices being so tiny that they're embedded into our eyeglasses, our earrings, or a tattoo on our forehead.

 

So the point of this album is to provide a frame of reference -- so that we can (hopefully) look back 10-20 years from now, and say, "Wasn't it really weird that we behaved in such bizarre ways while we interacted with those primitive devices?"

Tomé esta foto en una tienda donde hay mucha clientela maya de Guatemala, en el distrito de Fruitvale de Oakland, CA. Es buen lugar para ver la última moda en trajes típicos. Me pareció que esta mujer no hablaba mucho español, pero me dejó tomar su foto.

Su corte (falda) tiene franjas rojas en el urdimbre, un estilo nuevo, y ha hecho diseños geográficos nuevos en el corte y en el huipil. Todo cambia con estos trajes y el cambio es constante.

 

Tiene ropa tejida por ella misma en telares de cintura, menos la faja, que es computarizada, tristemente, y el rebozo, que fue tejido industrialmente, y luego una persona trenzó los flecos a mano. Lleva su bebé en el rebozo, y su celular en la faja, como siempre.

 

I took this picture in a store in Fruitvale, Oakland, CA, where there is lots of Guatemalan Maya clientele. She didn’t appear to speak much Spanish but she let me take her picture.

 

She has the same backstrap woven clothing as the others from this town, except the computerized belt :( unfortunately, and her shawl, which was industrially woven, then someone braided the fringe by hand. She carries her baby in that shawl and her cell phone in her belt, like all Maya women.

 

Santiago Chimaltenango, Huehuetenango, GUATEMALA (Mam) in Oakland, CA

Prod. 1981-1999/2001

Sn. 2475515

 

Top of the line 1981.

 

www.shootingfilm.net/2014/04/minolta-x-700-review.html

  

X-700 brochure:

"The X-700 is Minolta's fully-programmed, micro-computerized Automatic Exposure 35mm SLR. It's a simple-to-operate Automatic Exposure camera, selecting both aperture and shutter speed in Programmed Automatic Exposure mode (P mode). So all you have to do is focus-and-shoot. The X-700 also offers Aperture-Priority Automatic Exposure control (A mode) and a full-metered manual exposure control (M mode), in addition to many other features that make photography more fun and enjoyable than ever before."

 

wikipedia:

T"he Minolta X-700 is a 35 mm single-lens reflex film camera introduced by Minolta in 1981. It was the top model of their final manual-focus SLR series before the introduction of the auto-focus Minolta Maxxum 7000.

The X-700 was awarded the European "Camera of the Year" award in 1981, and its competitive pricing resulted in its becoming the most successful Minolta camera since the SRT line."

 

kenrockwell.com:

"A testament to its lasting and good design, it was introduced in the early 1980s and was in continuous production until the beginning of 2001. I had a very new one with a serial number above 3,000,000, and I also bought an X-570 (it's brother) back in 1982."

 

From x-700 owners manual:

Elecronically governed 35mm single-reflex AE camera.

Exposure-control modes:

Fully programmed (P), aperture-priority automatic (A), and metered manual (M).

Exposure control and functions:

Low-voltage, low current computer circuit incorporating quartz crystal for sequential control to 1/30,000-sec. accuracy, large-scale ICs, samarium-cobalt impulse-release magnets, and linear-resistance inputs) varies both aperture and shutter speed steplessly according to special "faster-speed" program in P mode, or varies shutter speed steplessly according to aperture set in A mode, to yield proper exposure for the film speed and exposure adjustment set; auto-exposure range: EV 1 to EV 18 (e.g., 1 sec. at f/1.4 to 1/1000 at f/16) at ISO 100/21° with f/1.4 lens; AE-lock device holds meter reading for exposure at that value regardless of subject-brightness changes.

Shutter:

Horizontal-traverse focal-plane type; electronically controlled stepless speeds 1/1000 to 4 sec. set automatically with endlessly rotatable selector dial locked at "P" or "A" setting or fixed speeds 1 to 1/1000 sec. or "B" (bulb) set manually at detented dial indications; electromagnetic shutter release locks when voltage too low for proper operation.

Metering:

TTL center-weighted averaging type, by silicon photocell mounted at rear of pentaprism for available light, measured full aperture for normal finder display, then at taking aperture for programmed/automatic-exposure setting/determination or stop-down display; by another SPC mounted with optic in side of mirror compartment for TTL off-film Direct Autoflash Metering at taking aperture during exposure to control burst duration of PX-series flash units.

Film-speed range:

ISO 25/150 to 1600/330 set by ASA dial that locks at 1/3-EV increments.

Exposure-adjustment control:

Up to ±2 EV continuous adjustment of P, A, or M exposure by dial that locks at zero position and each 1/2-EV setting.

Mirror:

Triple-coated oversize instant-return slide-up type.

Viewfinder:

Eye-Level fixed pentaprism type showing 95% of 24x36mm film-frame area; magnification: 02X with 50mm standard lens focused at infinity; power: -1D, adjustable with accessory Snap-On eyepiece lenses; Fresnel-field focusing screen having artificially regular-patterned matte field plus central split-image horizontally oriented focusing aid surrounded by microprism band, interchangeable with Type P1, P2, Pd, M, G, L, S, or H screens at authorized Minolta service stations; visible around frame: mode indication (P, A, or M), shutter-speed scale (1, 2, 4, 8, 15, 30, 60, 125, 250, 500, and 1000) with LED setting indication, triangular over-/under-range LED indicators blinking at 4Hz, flash-ready signal (LED next to "60" blinking at 2Hz), FDC signal ("60" LED blinking at 8Hz for 1 sec. after correct flash exposure), mis-set lens warning (mode indication blinking at 4Hz in P mode, battery check (by glowing of any LED when operating button touched or pressed slightly), f-number set with MD or MC lenses, and exposure-adjustment engaged indication (LED blinking at 4Hz); display and metering activated by normal finger contact or slight pressing of operating button and continue for 15 sec., except go out after shutter release.

Flash Sync and Control:

Hot shoe and PC terminal for X sync; camera-control contact on hot shoe for flash ready signaling and automatic setting of shutter at 1/60 sec. (except when mode/shutter-speed selector set for sync at "B") with PX and X flash units; other electronic units synchronize at 1/60 sec. and slower manual speeds or "B" setting; Class MF, M, and FP flashbulbs, at 1/15 sec. or slower settings; second contact on hot shoe for burst control by Direct Autoflash Metering with PX units.

Power:

Two 1.5v alkaline-manganese (LR44: Eveready A-76 or equiv.), two 1.55v silver-oxide (SR-44: Eveready S-76, EPX-76, or equiv.), or one 3v lithium (CR-1/3N) cell(s).

This image is dedicated to Mr. Pete Gordon and Mr. Dick Mann. They are the guys who are employed as Light Operators for the Niagara Falls Illumination Board. They have a combined 78 years of dedicated service.

 

Peter Gordon is 79 years old and in 2010 celebrated his 50th year of service.

Dick Mann is 77 years old and in 2010 celebrated his 28th year of service.

 

Both men work on alternating nights every day of every year, no matter the weather. They are the true artists who control the lights which shine upon the falls. The colors the Illumination lights use are white, red, amber, green, and blue.

 

There is no automated program which dictates the colour sequences that shine upon the Falls. The operator working creates the kaleidoscope of colours by calling upon their experience and artistic talents.

 

The Niagara Falls Illumination Board currently employ two operators on staff to conduct the nightly illumination of the Falls. The light show is controlled by a single operator, who changes colour of the lights by changing the combination of the coloured gelatins in front of each light. The standard colour of each light is white.

 

The entire operation is run from a small control panel in an elongated room overlooking the illumination lights with a vista of the American Falls and Horseshoe Falls. The operator will change the lights every five to ten minutes.

 

Until the Falls of 2009, the operator changed the light colours by manually turning a series of four colour coded (red, blue, green, yellow) round shaped toggle switches for each of the twenty-one lights. With each turn of any of these switches, a large coloured panel (or any combination of the four panels) housed in the section above the actual light drops down in front of the lights or rises as the case maybe in order to create the rainbows of colour shining upon the Falls.

 

In late 2009, the rectifier/control room was modernized. New modern and much smaller rectifiers were installed. These rectifiers are used to transform alternating current to direct current for the light projectors. The former light control panel was replaced with modern computerized "touch screen" activated screens. Touching the colours on the new computer screens automatically changes the gelatin colour panels in the light projectors.

 

The four primary gelatin colour panels (red, blue, purple, amber) are secured to 4 feet by four feet square metal panels within each projector light. It takes less than 30 seconds to change the colour of any light. The gelatin colour panels are replaced approximately four times a year and cost about $25 each.

 

The operator also controls the battery of three Xenon lights that were built to shine directly on the American Falls from a location along the Ontario Power Company access road on the Canadian by remote control.

 

Power is supplied by the City of Niagara Falls (Ontario) Hydro Commission. It is estimated that the cost of illuminating the Falls including the services of an operator is approximately $85 per hour.

 

More information can be found here:

www.niagarafrontier.com/illuminationlights.html

factoidz.com/niagara-falls-at-night-with-lights/

www.niagarafallstourism.com/

 

View on black

 

Canon 7d and 15-85 Lens Vanguard Tripod

Prod. 1981-1999/2001

Sn. 2475515

 

Top of the line 1981.

 

X-700 brochure:

"The X-700 is Minolta's fully-programmed, micro-computerized Automatic Exposure 35mm SLR. It's a simple-to-operate Automatic Exposure camera, selecting both aperture and shutter speed in Programmed Automatic Exposure mode (P mode). So all you have to do is focus-and-shoot. The X-700 also offers Aperture-Priority Automatic Exposure control (A mode) and a full-metered manual exposure control (M mode), in addition to many other features that make photography more fun and enjoyable than ever before."

 

wikipedia:

T"he Minolta X-700 is a 35 mm single-lens reflex film camera introduced by Minolta in 1981. It was the top model of their final manual-focus SLR series before the introduction of the auto-focus Minolta Maxxum 7000.

The X-700 was awarded the European "Camera of the Year" award in 1981, and its competitive pricing resulted in its becoming the most successful Minolta camera since the SRT line."

 

kenrockwell.com:

"A testament to its lasting and good design, it was introduced in the early 1980s and was in continuous production until the beginning of 2001. I had a very new one with a serial number above 3,000,000, and I also bought an X-570 (it's brother) back in 1982."

 

From x-700 owners manual:

Elecronically governed 35mm single-reflex AE camera.

Exposure-control modes:

Fully programmed (P), aperture-priority automatic (A), and metered manual (M).

Exposure control and functions:

Low-voltage, low current computer circuit incorporating quartz crystal for sequential control to 1/30,000-sec. accuracy, large-scale ICs, samarium-cobalt impulse-release magnets, and linear-resistance inputs) varies both aperture and shutter speed steplessly according to special "faster-speed" program in P mode, or varies shutter speed steplessly according to aperture set in A mode, to yield proper exposure for the film speed and exposure adjustment set; auto-exposure range: EV 1 to EV 18 (e.g., 1 sec. at f/1.4 to 1/1000 at f/16) at ISO 100/21° with f/1.4 lens; AE-lock device holds meter reading for exposure at that value regardless of subject-brightness changes.

Shutter:

Horizontal-traverse focal-plane type; electronically controlled stepless speeds 1/1000 to 4 sec. set automatically with endlessly rotatable selector dial locked at "P" or "A" setting or fixed speeds 1 to 1/1000 sec. or "B" (bulb) set manually at detented dial indications; electromagnetic shutter release locks when voltage too low for proper operation.

Metering:

TTL center-weighted averaging type, by silicon photocell mounted at rear of pentaprism for available light, measured full aperture for normal finder display, then at taking aperture for programmed/automatic-exposure setting/determination or stop-down display; by another SPC mounted with optic in side of mirror compartment for TTL off-film Direct Autoflash Metering at taking aperture during exposure to control burst duration of PX-series flash units.

Film-speed range:

ISO 25/150 to 1600/330 set by ASA dial that locks at 1/3-EV increments.

Exposure-adjustment control:

Up to ±2 EV continuous adjustment of P, A, or M exposure by dial that locks at zero position and each 1/2-EV setting.

Mirror:

Triple-coated oversize instant-return slide-up type.

Viewfinder:

Eye-Level fixed pentaprism type showing 95% of 24x36mm film-frame area; magnification: 02X with 50mm standard lens focused at infinity; power: -1D, adjustable with accessory Snap-On eyepiece lenses; Fresnel-field focusing screen having artificially regular-patterned matte field plus central split-image horizontally oriented focusing aid surrounded by microprism band, interchangeable with Type P1, P2, Pd, M, G, L, S, or H screens at authorized Minolta service stations; visible around frame: mode indication (P, A, or M), shutter-speed scale (1, 2, 4, 8, 15, 30, 60, 125, 250, 500, and 1000) with LED setting indication, triangular over-/under-range LED indicators blinking at 4Hz, flash-ready signal (LED next to "60" blinking at 2Hz), FDC signal ("60" LED blinking at 8Hz for 1 sec. after correct flash exposure), mis-set lens warning (mode indication blinking at 4Hz in P mode, battery check (by glowing of any LED when operating button touched or pressed slightly), f-number set with MD or MC lenses, and exposure-adjustment engaged indication (LED blinking at 4Hz); display and metering activated by normal finger contact or slight pressing of operating button and continue for 15 sec., except go out after shutter release.

Flash Sync and Control:

Hot shoe and PC terminal for X sync; camera-control contact on hot shoe for flash ready signaling and automatic setting of shutter at 1/60 sec. (except when mode/shutter-speed selector set for sync at "B") with PX and X flash units; other electronic units synchronize at 1/60 sec. and slower manual speeds or "B" setting; Class MF, M, and FP flashbulbs, at 1/15 sec. or slower settings; second contact on hot shoe for burst control by Direct Autoflash Metering with PX units.

Power:

Two 1.5v alkaline-manganese (LR44: Eveready A-76 or equiv.), two 1.55v silver-oxide (SR-44: Eveready S-76, EPX-76, or equiv.), or one 3v lithium (CR-1/3N) cell(s).

+++ 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!

Reprocessed M20 from 6/24/12. Still not great but I feel its better than the previous. Tighter & less stars,more blue reflection nebula

 

Orion ED102T CF Triplet Apochromatic Refractor Telescope.

Orion Sirius German-equatorial Computerized Goto Mount

 

Images aquired using APT

Guided with Starshoot Autoguider and 50mm guide scope

Aligned and stacked with Nebulosity

Post-process with StarTools GIMP & Windows Live Photo

 

33 total frames: (3hrs 19min)

4x300 7x600 1x720 iso 800 Canon T3(modified) with Astronomik Ha clip-in filter

5x300 2x600 iso 800 Canon T3(modified)with Astronomik CLS clip-in filter

6x120 8x300 iso 800 Canon T3i no filters

 

sites.google.com/site/astrochuck123

 

*****Check out my "terrestrial" pictures on:

www.flickr.com/photos/78400750@N07/

 

Reprocess in false color,with Ha as Green, OIII as Blue, Ha+RGB as Red.

 

Orion ED102T CF Triplet Apochromatic Refractor Telescope.-RGB & OIII

Orion ST-80T "guide scope"-Ha

Orion Sirius German-equatorial Computerized Goto Mount

Images aquired using APT

Guided with Starshoot Autoguider and 50mm guide scope

Aligned and stacked with Nebulosity

Post-process with StarTools GIMP & Windows Live Photo

 

38 total frames: (4hrs 35min) with an equal # of dark frames

OIII-4x300 5x600 iso 800 Canon T3i with Astronomik OIII clip-in filter

Ha-5x300 5x600 3x900 iso 800 Canon T3(modified) with Astronomik Ha clip-in filter

RGB-5x60 6x300 5x600 iso 800 Canon T3i no filters

 

sites.google.com/site/astrochuck123

 

*****Check out my "terrestrial" pictures on:

www.flickr.com/photos/78400750@N07/

 

Alfa Romeo 8C Competizione Spider (2008-10) Engine 4691cc V8 Ferrari-Alfa Romeo F136 YC V8

Production 1000 approx (500 Coupes, 500 Spiders)

Registration Number WX 12 BWZ (Bristol)

ALFA ROMEO SET

www.flickr.com/photos/45676495@N05/sets/72157623759785842...

 

Designed by Wolfgang Eggar at Centro Style Alfa Romeo the Alfa Romeo 8C Competizione was first presented as a concept car at the 2003 Frankfurt Motor Show and later offered for sale for the 2007 model year.The company received over 1,400 orders for the 8C after the official announcement that the car would enter production.[ However, only 500 customers ended up with the 8C Competizione and another 500 with the 8C Spider, bringing the production total to 1,000 cars.

 

The production version is very similar to the concept; the biggest difference to the exterior being the rear-hinged hood. while other changes included the front lights, which used Xenon lamps, a standard wiper system a side vent and wheels designed to echo images of the Alfa Romeo cloverleaf logo. The two seat carbon fibre body is fitted to a steel chassis, made by Italian company ITCA Produzione. Final assembly took place at the Maserati factory in Modena

 

The car uses a unique platform that shares several components with the Maserati GranTurismo. The powertrain features a Ferrari/Maserati derived cross-plane,[ wet sump lubricated 4.7 L (4,691 cc) 90° V8 engine assembled by Ferrari with an outpot of 444bhp The V8 engine has variable timing, intake valves and is mated to a six–speed transaxle gearbox with computerized gear selection by means of paddles on the steering column and may be used in Manual-Normal; Manual-Sport; Automatic-Normal; Automatic-Sport and Wet modes.

 

The Spider version was first shown at the 2005 Pebble Beach Concours d'Elegance, with the production version unveiled at the 2008 Geneva Motorshow with production begining in 2009. The limited number of 500 cars (35 of which were allocated to the USA) were priced at €199,000 (£174,000) excluding taxes.

 

Many thanks for a fantabulous

47,459,976 views

 

Shot at the NEC Classic Car Show 13:11:2015 Ref. 112-015

 

BF-4 Flt 509 Maj Michael Lippert and BF-5 Flt 371 Cdr Nathan Gray Test aboard HMS Queen Elizabeth on 28 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.

+++ 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.

 

Fotografia de la "Super Luna" tomada el dia 04/05/12. Como la Luna no entraba todo, la hice en 8 tomas, cada toma tiene 4300 imágenes superpuestas.

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