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The Arboretum has an interactive map on their web site. This map is found at the Arborway Gate.

 

Pasting from Wikipedia: Arnold Arboretum:

 

• • • • •

 

The Arnold Arboretum of Harvard University is an arboretum located in the Jamaica Plain and Roslindale sections of Boston, Massachusetts. It was designed by Frederick Law Olmsted and is the second largest "link" in the Emerald Necklace.

 

History

 

The Arboretum was founded in 1872 when the President and Fellows of Harvard College became trustees of a portion of the estate of James Arnold (1781–1868).

 

In 1842, Benjamin Bussey (1757–1842), a prosperous Boston merchant and scientific farmer, donated his country estate Woodland Hill and a part of his fortune to Harvard University "for instruction in agriculture, horticulture, and related subjects". Bussey had inherited land from fellow patriot Eleazer Weld in 1800 and further enlarged his large estate between 1806 and 1837 by acquiring and consolidating various farms that had been established as early as the seventeenth century. Harvard used this land for the creation of the Bussey Institute, which was dedicated to agricultural experimentation. The first Bussey Institute building was completed in 1871 and served as headquarters for an undergraduate school of agriculture.

 

Sixteen years after Bussey's death, James Arnold, a New Bedford, Massachusetts whaling merchant, specified that a portion of his estate was to be used for "...the promotion of Agricultural, or Horticultural improvements". In 1872, when the trustees of the will of James Arnold transferred his estate to Harvard University, Arnold’s gift was combined with 120 acres (0.49 km2) of the former Bussey estate to create the Arnold Arboretum. In the deed of trust between the Arnold trustees and the College, income from Arnold’s legacy was to be used for establishing, developing and maintaining an arboretum to be known as the Arnold Arboretum which "shall contain, as far as practicable, all the trees [and] shrubs ... either indigenous or exotic, which can be raised in the open air of West Roxbury". The historical mission of the Arnold Arboretum is to increase knowledge of woody plants through research and to disseminate this knowledge through education.

 

Charles Sprague Sargent was appointed director and Arnold Professor of Botany shortly after the establishment of the institution in 1872.[2] Together with landscape architect Frederick Law Olmsted he developed the road and pathway system and delineated the collection areas by family and genus, following the then current and widely accepted classification system of Bentham and Hooker. The Hunnewell building was designed by architect Alexander Wadsworth Longfellow, Jr. in 1892 and constructed with funds donated by H. H. Hunnewell in 1903. From 1946 to 1950 the landscape architect Beatrix Farrand was the landscape design consultant for the Arboretum. Her early training in the 1890s included time with Charles Sprague Sargent and chief propagator and superintendent Jackson Thornton Johnson.[3] Today the Arboretum occupies 265 acres (107 hectares) of land divided between four parcels, viz. the main Arboretum and the Peters Hill, Weld-Walter and South Street tracts. The collections, however, are located primarily in the main Arboretum and on the Peters Hill tract. The Arboretum remains one of the finest examples of a landscape designed by Frederick Law Olmsted and it is a Frederick Law Olmsted National Historic Site) and a National Historic Landmark.

 

Robert E. Cook is the seventh and current Director of the Arnold Arboretum. He is also the Director of the Harvard University Herbaria located in Cambridge, Massachusetts.

 

Status

 

The Arboretum is privately endowed as a department of Harvard University. The land, however, was deeded to the City of Boston in 1882 and incorporated into the so-called "Emerald Necklace". Under the agreement with the City, Harvard University was given a thousand-year lease on the property, and the University, as trustee, is directly responsible for the development, maintenance, and operation of the Arboretum; the City retains responsibility for water fountains, benches, roads, boundaries, and policing. The annual operating budget of $7,350,644 (fiscal year 2003) is largely derived from endowment, which is also managed by the University, and all Arboretum staff are University employees. Other income is obtained through granting agencies and contributors.

 

Location

 

The main Arborway gate is located on Route 203 a few hundred yards south of its junction with the Jamaicaway. Public transportation to the Arboretum is available on the MBTA Orange Line to its terminus at Forest Hills Station and by bus (#39) to the Monument in Jamaica Plain. The Arboretum is within easy walking distance from either of these points.

 

Hours

 

The grounds are open free of charge to the public from sunrise to sunset 365 days of the year. The Visitor's Center in the Hunnewell Building, 125 Arborway, is open Monday through Friday 9 a.m.–4 p.m.; Saturdays 10 a.m.–4 p.m.; Sundays 12 p.m.–4 PM. The Visitor’s Center is closed on holidays. The Library, located in the Hunnewell Building, is open Monday through Saturday, 10 a.m.–4 p.m.. The Library is closed on Sundays and holidays. Stacks are closed and the collection does not circulate.

 

Area

 

Two hundred and sixty-five acres (107 hectares) in the Jamaica Plain and Roslindale sections of Boston, Massachusetts, located at 42°19′N 71°5′W / 42.317°N 71.083°W / 42.317; -71.083, with altitudes ranging from 46 feet (15 m) in the meadow across the drive from the Hunnewell Building to 240 feet (79 m) at the top of Peters Hill.

 

Climate

 

Average yearly rainfall is 43.63 inches (1,102 mm); average snowfall, 40.2 inches (102 centimeters). Monthly mean temperature is 51.5 °F (10.8 °C); July's mean temperature is 73.5 °F (23 °C); January's is 29.6 °F (-1.3 °C). The Arboretum is located in USDA hardiness zone 6 (0 to −10 °F, −18 to −23 °C).

 

Collections (as of September 14, 2007)

 

At present, the living collections include 15,441 individual plants (including nursery holdings) belonging to 10,216 accessions representing 4,099 taxa; with particular emphasis on the ligneous species of North America and eastern Asia. Historic collections include the plant introductions from eastern Asia made by Charles Sprague Sargent, Ernest Henry Wilson, William Purdom, Joseph Hers, and Joseph Rock. Recent introductions from Asia have resulted from the 1977 Arnold Arboretum Expedition to Japan and Korea, the 1980 Sino-American Botanical Expedition to western Hubei Province, and more recent expeditions to China and Taiwan.

 

Comprehensive collections are maintained and augmented for most genera, and genera that have received particular emphasis include: Acer, Fagus, Carya, Forsythia, Taxodium, Pinus, Metasequoia, Lonicera, Magnolia, Malus, Quercus, Rhododendron, Syringa, Paulownia, Albizia, Ilex, Gleditsia and Tsuga. Other comprehensive collections include the Bradley Collection of Rosaceous Plants, the collection of conifers and dwarf conifers, and the Larz Anderson Bonsai Collection. Approximately 500 accessions are processed annually.

 

Collections policy

 

The mission of the Arnold Arboretum is to increase our knowledge of the evolution and biology of woody plants. Historically, this research has investigated the global distribution and evolutionary history of trees, shrubs and vines, with particular emphasis on the disjunct species of East Asia and North America. Today this work continues through molecular studies of the evolution and biogeography of the floras of temperate Asia, North America and Europe.

 

Research activities include molecular studies of gene evolution, investigations of plant-water relations, and the monitoring of plant phenology, vegetation succession, nutrient cycling and other factors that inform studies of environmental change. Applied work in horticulture uses the collections for studies in plant propagation, plant introduction, and environmental management. This diversity of scientific investigation is founded in a continuing commitment to acquire, grow, and document the recognized species and infraspecific taxa of ligneous plants of the Northern Hemisphere that are able to withstand the climate of the Arboretum’s 265-acre (1.07 km2) Jamaica Plain/Roslindale site.

 

As a primary resource for research in plant biology, the Arboretum’s living collections are actively developed, curated, and managed to support scientific investigation and study. To this end, acquisition policies place priority on obtaining plants that are genetically representative of documented wild populations. For each taxon, the Arnold Arboretum aspires to grow multiple accessions of known wild provenance in order to represent significant variation that may occur across the geographic range of the species. Accessions of garden or cultivated provenance are also acquired as governed by the collections policies herein.

 

For all specimens, full documentation of both provenance and history within the collection is a critical priority. Curatorial procedures provide for complete and accurate records for each accession, and document original provenance, locations in the collections, and changes in botanical identity. Herbarium specimens, DNA materials, and digital images are gathered for the collection and maintained in Arboretum data systems and the herbarium at the Roslindale site.

 

Research

 

Research on plant pathology and integrated pest management for maintenance of the living collections is constantly ongoing. Herbarium-based research focuses on the systematics and biodiversity of both temperate and tropical Asian forests, as well as the ecology and potential for sustainable use of their resources. The Arboretum's education programs offer school groups and the general public a wide range of lectures, courses, and walks focusing on the ecology and cultivation of plants. Its quarterly magazine, Arnoldia, provides in-depth information on horticulture, botany, and garden history. Current Research Initiatives

 

Plant Records

 

Plant records are maintained on a computerized database, BG-BASE 6.8 (BG-Base Inc.), which was initiated in 1985 at the request of the Arnold Arboretum and the Threatened Plants Unit (TPU) of the World Conservation Monitoring Centre (WCMC). A computerized mapping program (based on AutoCAD (Autodesk)) is linked to BG-BASE, and each accession is recorded on a series of maps at a scale of 1-inch (25 mm) to 20 feet (1:240) or 1-inch (25 mm) to 10 feet (1:120). A computer-driven embosser generates records labels. All accessioned plants in the collections are labeled with accession number, botanical name, and cultivar name (when appropriate), source information, common name, and map location. Trunk and/or display labels are also hung on many accessions and include botanical and common names and nativity. Stake labels are used to identify plants located in the Leventritt Garden and Chinese Path.

 

Grounds Maintenance

 

The grounds staff consists of the superintendent and assistant superintendent, three arborists, and ten horticultural technologists. A service garage is adjacent to the Hunnewell Building, where offices and locker rooms are located. During the summer months ten horticultural interns supplement the grounds staff. A wide array of vehicles and modern equipment, including an aerial lift truck and a John Deere backhoe and front loader, are used in grounds maintenance. Permanent grounds staff, excluding the superintendents, are members of AFL/CIO Local 615, Service Employees International Union (SEIU).

 

Nursery and Greenhouse Facilities

 

The Dana Greenhouses, located at 1050 Centre Street (with a mailing address of 125 Arborway), were completed in 1962. They comprise four service greenhouses totaling 3,744 square feet (348 m²), the headhouse with offices, cold rooms, storage areas, and a classroom. Staffing at the greenhouse includes the manager of greenhouses and nurseries, the plant propagator, two assistants, and, during the summer months, two horticultural interns. Adjacent to the greenhouse is a shade house of 3,150 square feet (293 m²), a 12,600 cubic foot (357 m³) cold storage facility, and three irrigated, inground nurseries totaling approximately one and one-half acres (6,000 m²). Also located in the greenhouse complex is the bonsai pavilion, where the Larz Anderson Bonsai Collection is displayed from the middle of April to the end of October. During the winter months the bonsai are held in the cold storage unit at temperatures slightly above freezing.

 

Isabella Welles Hunnewell Internship Program

 

The living collections department of the Arnold Arboretum offers a paid summer internship program [2] that combines hands-on training in horticulture with educational courses. Intern trainees will be accepted for 12- to 24-week appointments. Ten interns will work with the grounds maintenance department and two in the Dana Greenhouses.

 

As part of the training program, interns participate in mandatory instructional sessions and field trips in order to develop a broader sense of the Arboretum’s horticultural practices as well as those of other institutions. Sessions and field trips are led by Arnold staff members and embrace an open question and answer format encouraging all to participate. Interns often bring experience and knowledge that everyone, including staff, benefits from. It is a competitive-free learning environment.

 

Horticultural Apprenticeship

 

The Arboretum created the horticultural apprenticeship program in 1997 to provide hands-on experience in all aspects of the development, curation, and maintenance of the Arboretum's living collections to individuals interested in pursuing a career in an arboretum or botanical garden.

 

The Living Collections department of the Arnold Arboretum offers a summer internship program[4] that combines practical hands-on training in horticulture with educational courses. Fourteen Interns/Horticultural Trainees are accepted for twelve to twenty-four week appointments. Interns receive the majority of their training in one of three departments: Grounds Maintenance, Nursery and Greenhouse, or Plant Records.

 

Lilac Sunday

 

The second Sunday in May every year is "Lilac Sunday". This is the only day of the year that picnicing is allowed. In 2008, on the 100th anniversary of Lilac Sunday, the Arboretum website touted:

 

Of the thousands of flowering plants in the Arboretum, only one, the lilac, is singled out each year for a daylong celebration. On Lilac Sunday, garden enthusiasts from all over New England gather at the Arboretum to picnic, watch Morris dancing, and tour the lilac collection. On the day of the event, which takes place rain or shine, the Arboretum is open as usual from dawn to dusk.[5]

 

Associated Collections

 

The Arboretum's herbarium in Jamaica Plain holds specimens of cultivated plants that relate to the living collections (ca. 160,000). The Jamaica Plain herbarium, horticultural library, archives, and photographs are maintained in the Hunnewell building at 125 Arborway; however, the main portions of the herbarium and library collections are housed in Cambridge on the campus of Harvard University, at 22 Divinity Avenue.

 

Publications

 

The inventory of living collections is updated periodically and made available to sister botanical gardens and arboreta on request; it is also available on the Arboretum’s website (searchable inventory). Arnoldia, the quarterly magazine of the Arnold Arboretum, frequently publishes articles relating to the living collections. A Reunion of Trees[6] by Stephen A. Spongberg (curator emeritus) recounts the history of the introduction of many of the exotic species included in the Arobretum’s collections. New England Natives[7] written by horticultural research archivist Sheila Connor describes many of the trees and shrubs of the New England flora and the ways New Englanders have used them since prehistoric times. Science in the Pleasure Ground[8] by Ida Hay (former curatorial associate) constitutes an institutional biography of the Arboretum.

 

Institutional Collaborations

 

The Arboretum maintains an institutional membership in the American Public Garden Association (APGA) and the International Association of Botanical Gardens and Arboreta. Additionally, members of the staff are associated with many national and international botanical and horticultural organizations. The Arboretum is also a cooperating institution with the Center for Plant Conservation (CPC), and as an active member of the North American Plant Collections Consortium (NAPCC), it is committed to broadening and maintaining its holdings of: Acer, Carya, Fagus, Stewartia, Syringa, and Tsuga for the purposes of plant conservation, evaluation, and research. The Arboretum is also a member of the North American China Plant Exploration Consortium (NACPEC).

 

See also

 

Larz Anderson Bonsai Collection, donated by businessman and ambassador Larz Anderson

The Case Estates of the Arnold Arboretum

List of botanical gardens in the United States

North American Plant Collections Consortium

Adams-Nervine_Asylum

 

External links

 

Arnold Arboretum Official Website

Arnold Arboretum Visitor Information

Harvard University Herbaria

American Public Gardens Association (APGA)

Flora of China

Virtual Information Access (VIA) Catalog of visual resources at Harvard University.

Garden and Forest A Journal of Horticulture, Landscape Art, and Forestry (1888–1897)

Boston's Arnold Arboretum: A Place for Study and Recreation, a National Park Service Teaching with Historic Places (TwHP) lesson plan

The Emerald Necklace: Boston's Green Connection, a National Park Service Teaching with Historic Places (TwHP) lesson plan

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.

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.

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.

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.

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

Original Caption: Amtrak information and ticket counter in Chicago's Union Station, one of the busiest in the corporation's system. A nationwide computerized reservation system is modernizing the previously fragmented railroad information and ticketing procedures. Clerks at five major reservation centers, including Chicago, may consult computer-readout consoles for information on available space and fares, and quickly enter reservations, June 1974

  

U.S. National Archives’ Local Identifier: 412-DA-13619

 

Photographer: O'Rear, Charles, 1941-

  

Subjects:

Chicago (Illinois)

Environmental Protection Agency

Project DOCUMERICA

  

Persistent URL: research.archives.gov/description/556071

 

Repository: Still Picture Records Section, Special Media Archives Services Division (NWCS-S), National Archives at College Park, 8601 Adelphi Road, College Park, MD, 20740-6001.

 

For information about ordering reproductions of photographs held by the Still Picture Unit, visit: www.archives.gov/research/order/still-pictures.html

 

Reproductions may be ordered via an independent vendor. NARA maintains a list of vendors at www.archives.gov/research/order/vendors-photos-maps-dc.html

 

Access Restrictions: Unrestricted

Use Restrictions: Unrestricted

Port of Itajai

Vessel Berthed (Navio Atracado)

 

Vessel's Details (Detalhes do Navio)

Ship Type (tipo): Dry Cargo - Full Container

Year Built (ano de construção): 2001

Length x Breadth (Comprimento x Largura): 277 m X 40 m

DeadWeight (Tonelagem Bruta): 67591 t

Speed recorded (Max / Average) (Velocidade - máx /média): 12.3 / 7.6 knots

Call Sign: A8AV9

IMO: 9214226, MMSI: 636090586

 

Owner/Operator (Proprietário/Operador): MSC Mediterranean Shipping Co SA

Flag (Bandeira): Liberia

 

Berth (Berço): Portonave 01

A.T.B. (Atracação): April 06,2011 07:35h

E.T.D. (Previsão de saída): April 07,2011 08:00h

Agent (Agência): MSC

Origin (Origem): RIO DE JANEIRO (Brazil)

Destination (Destino): PARANAGUA (Brazil)

 

.

 

The Port of Itajai is a Brazilian port located in the City of Itajai, in the State of Santa Catarina, south Brazil.

 

This is the second largest port of Brazil in handling containers. It acts as export port and most of the Santa Catarina´s production passes through it.

 

The port of Itajai has over 15,000 m2 of covered area to warehouse products and 38,000 m2 of open area to warehouse containers. The users of the Itajai Port have at their disposal over 70 equipments to assist loadings and unloadings of 1 to 37 tons.

 

The port follows international safety standards. The operational units are fully computerized.

 

In 2010, the Port of Itajai handled a total of 954.38 thousand TEUs (Twenty-foot Equivalent Unit – international unit equivalent to a 20-foot container). Over 1.25 thousand vessels called at the Port of Itajai, including cargo and passenger vessels.

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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...

+++ 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 OV-10 Bronco was initially conceived in the early 1960s through an informal collaboration between W. H. Beckett and Colonel K. P. Rice, U.S. Marine Corps, who met at Naval Air Weapons Station China Lake, California, and who also happened to live near each other. The original concept was for a rugged, simple, close air support aircraft integrated with forward ground operations. At the time, the U.S. Army was still experimenting with armed helicopters, and the U.S. Air Force was not interested in close air support.

The concept aircraft was to operate from expedient forward air bases using roads as runways. Speed was to be from very slow to medium subsonic, with much longer loiter times than a pure jet. Efficient turboprop engines would give better performance than piston engines. Weapons were to be mounted on the centerline to get efficient aiming. The inventors favored strafing weapons such as self-loading recoilless rifles, which could deliver aimed explosive shells with less recoil than cannons, and a lower per-round weight than rockets. The airframe was to be designed to avoid the back blast.

 

Beckett and Rice developed a basic platform meeting these requirements, then attempted to build a fiberglass prototype in a garage. The effort produced enthusiastic supporters and an informal pamphlet describing the concept. W. H. Beckett, who had retired from the Marine Corps, went to work at North American Aviation to sell the aircraft.

The aircraft's design supported effective operations from forward bases. The OV-10 had a central nacelle containing a crew of two in tandem and space for cargo, and twin booms containing twin turboprop engines. The visually distinctive feature of the aircraft is the combination of the twin booms, with the horizontal stabilizer that connected them at the fin tips. The OV-10 could perform short takeoffs and landings, including on aircraft carriers and large-deck amphibious assault ships without using catapults or arresting wires. Further, the OV-10 was designed to take off and land on unimproved sites. Repairs could be made with ordinary tools. No ground equipment was required to start the engines. And, if necessary, the engines would operate on high-octane automobile fuel with only a slight loss of power.

 

The aircraft had responsive handling and could fly for up to 5½ hours with external fuel tanks. The cockpit had extremely good visibility for both pilot and co-pilot, provided by a wrap-around "greenhouse" that was wider than the fuselage. North American Rockwell custom ejection seats were standard, with many successful ejections during service. With the second seat removed, the OV-10 could carry 3,200 pounds (1,500 kg) of cargo, five paratroopers, or two litter patients and an attendant. Empty weight was 6,969 pounds (3,161 kg). Normal operating fueled weight with two crew was 9,908 pounds (4,494 kg). Maximum takeoff weight was 14,446 pounds (6,553 kg).

The bottom of the fuselage bore sponsons or "stub wings" that improved flight performance by decreasing aerodynamic drag underneath the fuselage. Normally, four 7.62 mm (.308 in) M60C machine guns were carried on the sponsons, accessed through large forward-opening hatches. The sponsons also had four racks to carry bombs, pods, or fuel. The wings outboard of the engines contained two additional hardpoints, one per side. Racked armament in the Vietnam War was usually seven-shot 2.75 in (70 mm) rocket pods with white phosphorus marker rounds or high-explosive rockets, or 5" (127 mm) four-shot Zuni rocket pods. Bombs, ADSIDS air-delivered/para-dropped unattended seismic sensors, Mk-6 battlefield illumination flares, and other stores were also carried.

Operational experience showed some weaknesses in the OV-10's design. It was significantly underpowered, which contributed to crashes in Vietnam in sloping terrain because the pilots could not climb fast enough. While specifications stated that the aircraft could reach 26,000 feet (7,900 m), in Vietnam the aircraft could reach only 18,000 feet (5,500 m). Also, no OV-10 pilot survived ditching the aircraft.

 

The OV-10 served in the U.S. Air Force, U.S. Marine Corps, and U.S. Navy, as well as in the service of a number of other countries. In U.S. military service, the Bronco was operated until the early Nineties, and obsoleted USAF OV-10s were passed on to the Bureau of Alcohol, Tobacco, and Firearms for anti-drug operations. A number of OV-10As furthermore ended up in the hands of the California Department of Forestry (CDF) and were used for spotting fires and directing fire bombers onto hot spots.

 

This was not the end of the OV-10 in American military service, though: In 2012, the type gained new attention because of its unique qualities. A $20 million budget was allocated to activate an experimental USAF unit of two airworthy OV-10Gs, acquired from NASA and the State Department. These machines were retrofitted with military equipment and were, starting in May 2015, deployed overseas to support Operation “Inherent Resolve”, flying more than 120 combat sorties over 82 days over Iraq and Syria. Their concrete missions remained unclear, and it is speculated they provided close air support for Special Forces missions, esp. in confined urban environments where the Broncos’ loitering time and high agility at low speed and altitude made them highly effective and less vulnerable than helicopters.

Furthermore, these Broncos reputedly performed strikes with the experimental AGR-20A “Advanced Precision Kill Weapons System (APKWS)”, a Hydra 70-millimeter rocket with a laser-seeking head as guidance - developed for precision strikes against small urban targets with little collateral damage. The experiment ended satisfactorily, but the machines were retired again, and the small unit was dissolved.

 

However, the machines had shown their worth in asymmetric warfare, and the U.S. Air Force decided to invest in reactivating the OV-10 on a regular basis, despite the overhead cost of operating an additional aircraft type in relatively small numbers – but development and production of a similar new type would have caused much higher costs, with an uncertain time until an operational aircraft would be ready for service. Re-activating a proven design and updating an existing airframe appeared more efficient.

The result became the MV-10H, suitably christened “Super Bronco” but also known as “Black Pony”, after the program's internal name. This aircraft was derived from the official OV-10X proposal by Boeing from 2009 for the USAF's Light Attack/Armed Reconnaissance requirement. Initially, Boeing proposed to re-start OV-10 manufacture, but this was deemed uneconomical, due to the expected small production number of new serial aircraft, so the “Black Pony” program became a modernization project. In consequence, all airframes for the "new" MV-10Hs were recovered OV-10s of various types from the "boneyard" at Davis-Monthan Air Force Base in Arizona.

 

While the revamped aircraft would maintain much of its 1960s-vintage rugged external design, modernizations included a completely new, armored central fuselage with a highly modified cockpit section, ejection seats and a computerized glass cockpit. The “Black Pony” OV-10 had full dual controls, so that either crewmen could steer the aircraft while the other operated sensors and/or weapons. This feature would also improve survivability in case of incapacitation of a crew member as the result from a hit.

The cockpit armor protected the crew and many vital systems from 23mm shells and shrapnel (e. g. from MANPADS). The crew still sat in tandem under a common, generously glazed canopy with flat, bulletproof panels for reduced sun reflections, with the pilot in the front seat and an observer/WSO behind. The Bronco’s original cargo capacity and the rear door were retained, even though the extra armor and defensive measures like chaff/flare dispensers as well as an additional fuel cell in the central fuselage limited the capacity. However, it was still possible to carry and deploy personnel, e. g. small special ops teams of up to four when the aircraft flew in clean configuration.

Additional updates for the MV-10H included structural reinforcements for a higher AUW and higher g load maneuvers, similar to OV-10D+ standards. The landing gear was also reinforced, and the aircraft kept its ability to operate from short, improvised airstrips. A fixed refueling probe was added to improve range and loiter time.

 

Intelligence sensors and smart weapon capabilities included a FLIR sensor and a laser range finder/target designator, both mounted in a small turret on the aircraft’s nose. The MV-10H was also outfitted with a data link and the ability to carry an integrated targeting pod such as the Northrop Grumman LITENING or the Lockheed Martin Sniper Advanced Targeting Pod (ATP). Also included was the Remotely Operated Video Enhanced Receiver (ROVER) to provide live sensor data and video recordings to personnel on the ground.

 

To improve overall performance and to better cope with the higher empty weight of the modified aircraft as well as with operations under hot-and-high conditions, the engines were beefed up. The new General Electric CT7-9D turboprop engines improved the Bronco's performance considerably: top speed increased by 100 mph (160 km/h), the climb rate was tripled (a weak point of early OV-10s despite the type’s good STOL capability) and both take-off as well as landing run were almost halved. The new engines called for longer nacelles, and their circular diameter markedly differed from the former Garrett T76-G-420/421 turboprop engines. To better exploit the additional power and reduce the aircraft’s audio signature, reversible contraprops, each with eight fiberglass blades, were fitted. These allowed a reduced number of revolutions per minute, resulting in less noise from the blades and their tips, while the engine responsiveness was greatly improved. The CT7-9Ds’ exhausts were fitted with muzzlers/air mixers to further reduce the aircraft's noise and heat signature.

Another novel and striking feature was the addition of so-called “tip sails” to the wings: each wingtip was elongated with a small, cigar-shaped fairing, each carrying three staggered, small “feather blade” winglets. Reputedly, this installation contributed ~10% to the higher climb rate and improved lift/drag ratio by ~6%, improving range and loiter time, too.

Drawing from the Iraq experience as well as from the USMC’s NOGS test program with a converted OV-10D as a night/all-weather gunship/reconnaissance platform, the MV-10H received a heavier gun armament: the original four light machine guns that were only good for strafing unarmored targets were deleted and their space in the sponsons replaced by avionics. Instead, the aircraft was outfitted with a lightweight M197 three-barrel 20mm gatling gun in a chin turret. This could be fixed in a forward position at high speed or when carrying forward-firing ordnance under the stub wings, or it could be deployed to cover a wide field of fire under the aircraft when it was flying slower, being either slaved to the FLIR or to a helmet sighting auto targeting system.

The original seven hardpoints were retained (1x ventral, 2x under each sponson, and another pair under the outer wings), but the total ordnance load was slightly increased and an additional pair of launch rails for AIM-9 Sidewinders or other light AAMs under the wing tips were added – not only as a defensive measure, but also with an anti-helicopter role in mind; four more Sidewinders could be carried on twin launchers under the outer wings against aerial targets. Other guided weapons cleared for the MV-10H were the light laser-guided AGR-20A and AGM-119 Hellfire missiles, the Advanced Precision Kill Weapon System upgrade to the light Hydra 70 rockets, the new Laser Guided Zuni Rocket which had been cleared for service in 2010, TV-/IR-/laser-guided AGM-65 Maverick AGMs and AGM-122 Sidearm anti-radar missiles, plus a wide range of gun and missile pods, iron and cluster bombs, as well as ECM and flare/chaff pods, which were not only carried defensively, but also in order to disrupt enemy ground communication.

 

In this configuration, a contract for the conversion of twelve mothballed American Broncos to the new MV-10H standard was signed with Boeing in 2016, and the first MV-10H was handed over to the USAF in early 2018, with further deliveries lasting into early 2020. All machines were allocated to the newly founded 919th Special Operations Support Squadron at Duke Field (Florida). This unit was part of the 919th Special Operations Wing, an Air Reserve Component (ARC) of the United States Air Force. It was assigned to the Tenth Air Force of Air Force Reserve Command and an associate unit of the 1st Special Operations Wing, Air Force Special Operations Command (AFSOC). If mobilized the wing was gained by AFSOC (Air Force Special Operations Command) to support Special Tactics, the U.S. Air Force's special operations ground force. Similar in ability and employment to Marine Special Operations Command (MARSOC), U.S. Army Special Forces and U.S. Navy SEALs, Air Force Special Tactics personnel were typically the first to enter combat and often found themselves deep behind enemy lines in demanding, austere conditions, usually with little or no support.

 

The MV-10Hs are expected to provide support for these ground units in the form of all-weather reconnaissance and observation, close air support and also forward air control duties for supporting ground units. Precision ground strikes and protection from enemy helicopters and low-flying aircraft were other, secondary missions for the modernized Broncos, which are expected to serve well into the 2040s. Exports or conversions of foreign OV-10s to the Black Pony standard are not planned, though.

  

General characteristics:

Crew: 2

Length: 42 ft 2½ in (12,88 m) incl. pitot

Wingspan: 45 ft 10½ in(14 m) incl. tip sails

Height: 15 ft 2 in (4.62 m)

Wing area: 290.95 sq ft (27.03 m²)

Airfoil: NACA 64A315

Empty weight: 9,090 lb (4,127 kg)

Gross weight: 13,068 lb (5,931 kg)

Max. takeoff weight: 17,318 lb (7,862 kg)

 

Powerplant:

2× General Electric CT7-9D turboprop engines, 1,305 kW (1,750 hp) each,

driving 8-bladed Hamilton Standard 8 ft 6 in (2.59 m) diameter constant-speed,

fully feathering, reversible contra-rotating propellers with metal hub and composite blades

 

Performance:

Maximum speed: 390 mph (340 kn, 625 km/h)

Combat range: 198 nmi (228 mi, 367 km)

Ferry range: 1,200 nmi (1,400 mi, 2,200 km) with auxiliary fuel

Maximum loiter time: 5.5 h with auxiliary fuel

Service ceiling: 32.750 ft (10,000 m)

13,500 ft (4.210 m) on one engine

Rate of climb: 17.400 ft/min (48 m/s) at sea level

Take-off run: 480 ft (150 m)

740 ft (227 m) to 50 ft (15 m)

1,870 ft (570 m) to 50 ft (15 m) at MTOW

Landing run: 490 ft (150 m)

785 ft (240 m) at MTOW

1,015 ft (310 m) from 50 ft (15 m)

 

Armament:

1x M197 3-barreled 20 mm Gatling cannon in a chin turret with 750 rounds ammo capacity

7x hardpoints for a total load of 5.000 lb (2,270 kg)

2x wingtip launch rails for AIM-9 Sidewinder AAMs

  

The kit and its assembly:

This fictional Bronco update/conversion was simply spawned by the idea: could it be possible to replace the original cockpit section with one from an AH-1 Cobra, for a kind of gunship version?

 

The basis is the Academy OV-10D kit, mated with the cockpit section from a Fujimi AH-1S TOW Cobra (Revell re-boxing, though), chosen because of its “boxy” cockpit section with flat glass panels – I think that it conveys the idea of an armored cockpit section best. Combining these parts was not easy, though, even though the plan sound simple. Initially, the Bronco’s twin booms, wings and stabilizer were built separately, because this made PSR on these sections easier than trying the same on a completed airframe. One of the initial challenges: the different engines. I wanted something uprated, and a different look, and I had a pair of (excellent!) 1:144 resin engines from the Russian company Kompakt Zip for a Tu-95 bomber at hand, which come together with movable(!) eight-blade contraprops that were an almost perfect size match for the original three-blade props. Biggest problem: the Tu-95 nacelles have a perfectly circular diameter, while the OV-10’s booms are square and rectangular. Combining these parts and shapes was already a messy PST affair, but it worked out quite well – even though the result rather reminds of some Chinese upgrade measure (anyone know the Tu-4 copies with turboprops? This here looks similar!). But while not pretty, I think that the beafier look works well and adds to the idea of a “revived” aircraft. And you can hardly beat the menacing look of contraprops on anything...

The exotic, so-called “tip sails” on the wings, mounted on short booms, are a detail borrowed from the Shijiazhuang Y-5B-100, an updated Chinese variant/copy of the Antonov An-2 biplane transporter. The booms are simple pieces of sprue from the Bronco kit, the winglets were cut from 0.5mm styrene sheet.

 

For the cockpit donor, the AH-1’s front section was roughly built, including the engine section (which is a separate module, so that the basic kit can be sold with different engine sections), and then the helicopter hull was cut and trimmed down to match the original Bronco pod and to fit under the wing. This became more complicated than expected, because a) the AH-1 cockpit and the nose are considerably shorter than the OV-10s, b) the AH-1 fuselage is markedly taller than the Bronco’s and c) the engine section, which would end up in the area of the wing, features major recesses, making the surface very uneven – calling for massive PSR to even this out. PSR was also necessary to hide the openings for the Fujimi AH-1’s stub wings. Other issues: the front landing gear (and its well) had to be added, as well as the OV-10 wing stubs. Furthermore, the new cockpit pod’s rear section needed an aerodynamical end/fairing, but I found a leftover Academy OV-10 section from a build/kitbashing many moons ago. Perfect match!

All these challenges could be tackled, even though the AH-1 cockpit looks surprisingly stout and massive on the Bronco’s airframe - the result looks stockier than expected, but it works well for the "Gunship" theme. Lots of PSR went into the new central fuselage section, though, even before it was mated with the OV-10 wing and the rest of the model.

Once cockpit and wing were finally mated, the seams had to disappear under even more PSR and a spinal extension of the canopy had to be sculpted across the upper wing surface, which would meld with the pod’s tail in a (more or less) harmonious shape. Not an easy task, and the fairing was eventually sculpted with 2C putty, plus even more PSR… Looks quite homogenous, though.

 

After this massive body work, other hardware challenges appeared like small distractions. The landing gear was another major issue because the deeper AH-1 section lowered the ground clearance, also because of the chin turret. To counter this, I raised the OV-10’s main landing gear by ~2mm – not much, but it was enough to create a credible stance, together with the front landing gear transplant under the cockpit, which received an internal console to match the main landing gear’s length. Due to the chin turret and the shorter nose, the front wheel retracts backwards now. But this looks quite plausible, thanks to the additional space under the cockpit tub, which also made a belt feed for the gun’s ammunition supply believable.

To enhance the menacing look I gave the model a fixed refueling boom, made from 1mm steel wire and a receptor adapter sculpted with white glue. The latter stuff was also used add some antenna fairings around the hull. Some antennae, chaff dispensers and an IR decoy were taken from the Academy kit.

 

The ordnance came from various sources. The Sidewinders under the wing tips were taken from an Italeri F-16C/D kit, they look better than the missiles from the Academy Bronco kit. Their launch rails came from an Italeri Bae Hawk 200. The quadruple Hellfire launchers on the underwing hardpoints were left over from an Italeri AH-1W, and they are a perfect load for this aircraft and its role. The LAU-10 and -19 missile pods on the stub wings were taken from the OV-10 kit.

  

Painting and markings:

Finding a suitable and somewhat interesting – but still plausible – paint scheme was not easy. Taking the A-10 as benchmark, an overall light grey livery (with focus on low contrast against the sky as protection against ground fire) would have been a likely choice – and in fact the last operational American OV-10s were painted in this fashion. But in order to provide a different look I used the contemporary USAF V-22Bs and Special Operations MC-130s as benchmark, which typically carry a darker paint scheme consisting of FS 36118 (suitably “Gunship Gray” :D) from above, FS 36375 underneath, with a low, wavy waterline, plus low-viz markings. Not spectacular, but plausible – and very similar to the late r/w Colombian OV-10s.

The cockpit tub became Dark Gull Grey (FS 36231, Humbrol 140) and the landing gear white (Revell 301).

 

The model received an overall black ink washing and some post-panel-shading, to liven up the dull all-grey livery. The decals were gathered from various sources, and I settled for black USAF low-viz markings. The “stars and bars” come from a late USAF F-4, the “IP” tail code was tailored from F-16 markings and the shark mouth was taken from an Academy AH-64. Most stencils came from another Academy OV-10 sheet and some other sources.

Decals were also used to create the trim on the propeller blades and markings on the ordnance.

 

Finally, the model was sealed with a coat of matt acrylic varnish (Italeri) and some exhaust soot stains were added with graphite along the tail boom flanks.

  

A successful transplantation – but is this still a modified Bronco or already a kitbashing? The result looks quite plausible and menacing, even though the TOW Cobra front section appears relatively massive. But thanks to the bigger engines and extended wing tips the proportions still work. The large low-pressure tires look a bit goofy under the aircraft, but they are original. The grey livery works IMHO well, too – a more colorful or garish scheme would certainly have distracted from the modified technical basis.

+++ DISCLAIMER +++

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

  

Some background:

The Georgian Air Force and Air Defense Division (თავდაცვის ძალების ავიაციისა და საჰაერო თავდაცვის სარდლობა; tavdatsvis dzalebis aviatsiisa da sahaero tavdatsvis sardloba) was established on January 1, 1992, and in September the Georgian Air Force conducted its first combat flight during the separatist war in Abkhazia. On August 18, 1998, the two divisions were unified in a joint command structure and renamed the Georgian Air Force.

In 2010, the Georgian Air Force was abolished as a separate branch and incorporated into the Georgian Land Forces as Air and Air Defense sections. By that time, the equipment – primarily consisting of Eastern Bloc aircraft inherited from the Soviet Union after the country’s dissolution – was totally outdated, the most potent aircraft were a dozen Suchoj Su-25 attack aircraft and a handful of MiG-21U trainers.

 

In order to rejuvenate the air arm, Tbilisi Aircraft Manufacturing (TAM), also known as JSC Tbilaviamsheni and formerly known as 31st aviation factory, started a modernization program for the Su-25, for the domestic forces but also for export customers. TAM had a long tradition of aircraft production within the Soviet Union. In the 1950s the factory started the production of Mikoyan's MiG-15 and later, the MiG-17 fighter aircraft. In 1957 Tbilisi Aircraft State Association built the MiG-21 two-seater fighter-trainer aircraft and its various derivative aircraft, continuing the MiG-21 production for about 25 years. At the same time the company was manufacturing the K-10 air-to-surface guided missile. Furthermore, the first Sukhoi Su-25 (known in the West as the "Frogfoot") close support aircraft took its maiden voyage from the runway of 31st aviation factory. Since then, more than 800 SU-25s had been delivered to customers worldwide. From the first SU-25 to the 1990s, JSC Tbilaviamsheni was the only manufacturer of this aircraft, and even after the fall of the Soviet Union the production lines were still intact and spares for more than fifty complete aircraft available. Along with the SU-25 aircraft 31st aviation factory also launched large-scale production of air-to-air R-60 and R-73 IR guided missiles, a production effort that built over 6,000 missiles a year and that lasted until the early 1990s. From 1996 to 1998 the factory also produced Su-25U two-seaters.

 

In 2001 the factory started, in partnership with Elbit Systems of Israel, upgrading basic Su-25 airframes to the Su-25KM “Scorpion” variant. This was just a technical update, however, intended for former Su-25 export customers who would upgrade their less potent Su-25K export aircraft with modern avionics. The prototype aircraft made its maiden flight on 18 April 2001 at Tbilisi in full Georgian Air Force markings. The aircraft used a standard Su-25 airframe, enhanced with advanced avionics including a glass cockpit, digital map generator, helmet-mounted display, computerized weapons system, complete mission pre-plan capability, and fully redundant backup modes. Performance enhancements included a highly accurate navigation system, pinpoint weapon delivery systems, all-weather and day/night performance, NATO compatibility, state-of-the art safety and survivability features, and advanced onboard debriefing capabilities complying with international requirements. The Su-25KM had the ability to use NATO-standard Mark 82 and Mark 83 laser-guided bombs and new air-to-air missiles, the short-range Vympel R-73. This upgrade extended service life of the Su-25 airframes for another decade.

There were, however, not many customers. Manufacturing was eventually stopped at the end of 2010, after Georgian air forces have been permanently dismissed and abolished. By that time, approximately 12 Scorpions had been produced, but the Georgian Air Force still used the basic models of Su-25 because of high cost of Su-25KM and because it was destined mainly for export. According to unofficial sources several Scorpions had been transferred to Turkmenistan as part of a trade deal.

 

In the meantime, another, more ambitious project took shape at Tbilisi Aircraft Manufacturing, too: With the help of Israel Aircraft Industries (IAI) the company started the development of a completely new attack aircraft, the TAM-1 “Gvelgeslas” (გველგესლას, Viper). It heavily relied on the year-long experience gathered with Su-25 production at Tblisi and on the tools at hand, but it was eventually a completely new aircraft – looking like a crossbreed between the Su-25 and the American A-10 with a T-tail.

 

This new layout had become necessary because the aircraft was to be powered by more modern, less noisy and more fuel-efficient Rolls Royce AE 3012 turbofan engines - which were originally intended to power the stillborn Yakovlev Yak-77 twin-engine business jet for up to 32 passengers, a slightly derated variant of the GMA 3012 with a 44 in diameter (112 cm) fan and procured via IAI from the United States through the company’s connection with Gulfstream Aerospace. Their larger diameter (the Su-25’s original Soyuz/Tumansky R-195 turbojets had a diameter of 109,5 cm/43.1 in) precluded the use of the former integral engine nacelles along the fuselage. To keep good ground clearance against FOD and to protect them from small arms fire, the engine layout was completely re-arranged. The fuselage was streamlined, and its internal structure was totally changed. The wings moved into a low position. The wings’ planform was almost identical to the Su-25’s, together with the characteristic tip-mounted “crocodile” air brakes. Just the leading edge inside of the “dogteeth” and the wing roots were re-designed, the latter because of the missing former engine nacelles. This resulted in a slightly increased net area, the original wingspan was retained. The bigger turbofans were then mounted in separate pods on short pylons along the rear fuselage, partly protected from below by the wings. Due to the jet efflux and the engines’ proximity to the stabilizers, these were re-located to the top of a deeper, reinforced fin for a T-tail arrangement.

 

Since the Su-25’s engine bays were now gone, the main landing gear had to be completely re-designed. Retracting them into the fuselage or into the relatively thin wings was not possible, TAM engineers settled upon a design that was very similar to the A-10: the aircraft received streamlined fairings, attached to the wings’ main spar, and positioned under the wings’ leading edges. The main legs were only semi-retractable; in flight, the wheels partly protruded from the fairings, but that hardly mattered from an aerodynamic point of view at the TAM-1’s subsonic operational speed. As a bonus they could still be used while retracted during emergency landings, improving the aircraft’s crash survivability.

 

Most flight and weapon avionics were procured from or via Elbit, including the Su-25KT’s modernized “glass cockpit”, and the TAM-1’s NATO compatibility was enhanced to appeal to a wider international export market. Beyond a total of eleven hardpoints under the wings and the fuselage for an external ordnance of up to 4.500 kg (9.900 lb), the TAM-1 was furthermore armed with an internal gun. Due to procurement issues, however, the Su-25’s original twin-barrel GSh-30-2 was replaced with an Oerlikon KDA 35mm cannon – a modern variant of the same cannon used in the German Gepard anti-aircraft tank, adapted to the use in an aircraft with a light-weight gun carriage. The KDA gun fired with a muzzle velocity of 1,440 m/s (4,700 ft/s) and a range of 5.500m, its rate of fire was typically 550 RPM. For the TAM-1, a unique feature from the SPAAG installation was adopted: the gun had two magazines, one with space for 200 rounds and another, smaller one for 50. The magazines could be filled with different types of ammunition, and the pilot was able select between them with a simple switch, adapting to the combat situation. Typical ammunition types were armor-piercing FAPDS rounds against hardened ground targets like tanks, and high explosive shells against soft ground targets and aircraft or helicopters, in a 3:1 ratio. Other ammunition types were available, too, and only 200 rounds were typically carried for balance reasons.

 

The TAM-1’s avionics included a SAGEM ULISS 81 INS, a Thomson-CSF VE-110 HUD, a TMV630 laser rangefinder in a modified nose and a TRT AHV 9 radio altimeter, with all avionics linked through a digital MIL-STD-1553B data bus and a modern “glass cockpit”. A HUD was standard, but an Elbit Systems DASH III HMD could be used by the pilot, too. The DASH GEN III was a wholly embedded design, closely integrated with the aircraft's weapon system, where the complete optical and position sensing coil package was built within the helmet (either the USAF standard HGU-55/P or the Israeli standard HGU-22/P), using a spherical visor to provide a collimated image to the pilot. A quick-disconnect wire powered the display and carried video drive signals to the helmet's Cathode Ray Tube (CRT).

 

The TAM-1’s development was long and protracted, though, primarily due to lack of resources and the fact that the Georgian air force was in an almost comatose state for several years, so that the potential prime customer for the TAM-1 was not officially available. However, the first TAM-1 prototype eventually made its maiden flight in September 2017. This was just in time, because the Georgian Air Force had formally been re-established in 2016, with plans for a major modernization and procurement program. Under the leadership of Georgian Minister of Defense Irakli Garibashvili the Air Force was re-prioritized and aircraft owned by the Georgian Air Force were being modernized and re-serviced after they were left abandoned for 4 years. This program lasted until 2020. In order to become more independent from foreign sources and support its domestic aircraft industry, the Georgian Air Force eventually ordered eight TAM-1s as Su-25K replacements, which would operate alongside a handful of modernized Su-25KMs from national stock. In the meantime, the new type also attained interest from abroad, e. g. from Bulgaria, the Congo and Cyprus. The IDF thoroughly tested two early production TAM-1s of the Georgian Air Force in 2018, too.

  

General characteristics:

Crew: 1

Length: 15.53 m (50 ft 11 in), including pitot

Wingspan: 14.36 m (47 ft 1 in)

Height: 4.8 m (15 ft 9 in)

Wing area: 35.2 m² (378 sq ft)

Empty weight: 9,800 kg (21,605 lb)

Gross weight: 14,440 kg (31,835 lb)

Max takeoff weight: 19,300 kg (42,549 lb)

 

Powerplant:

2× Rolls-Royce AE 3012 turbofans with 44.1 kN (9,920 lbf) thrust each

 

Performance:

Maximum speed: 975 km/h (606 mph, 526 kn, Mach 0.79)

Range: 1.000 km (620 mi, 540 nmi) with internal fuel, clean

Combat range: 750 km (470 mi, 400 nmi) at sea level with 4.500 kg (9,911 lb) of ordnance,

incl. two external fuel tanks

Service ceiling: 7.800 m (25,550 ft)

g limits: +6.5

Rate of climb: 58 m/s (11,400 ft/min)

 

Armament:

1× 35 mm (1.38 in) Oerlikon KDA cannon with 200 rds in two magazines

under the lower forward fuselage, offset to port side.

11× hardpoints with a capacity of up to 4.500 kg (9,911 lb) of external stores

  

The kit and its assembly:

This rather rigorous conversion had been on my project list for many years, and with the “Gunships” group build at whatifmodellers.com in late 2021 I eventually gathered my mojo to tackle it. The ingredients had already been procured long ago, but there are ideas that make you think twice before you take action…

 

This build was somewhat inspired by a CG rendition of a modified Su-25 that I came across while doing online search for potential ideas, running under the moniker “Su-125”, apparently created by someone called “Bispro” and published at DeviantArt in 2010; check this: (www.deviantart.com/bispro/art/Sukhoi-Su-125-Foghorn-15043...). The rendition shows a Su-25 with its engines re-located to the rear fuselage in separate nacelles, much like an A-10, plus a T-tail. However, as many photoshopped aircraft, the shown concept had IMHO some flaws. Where would a landing gear go, as the Su-125 still had shoulder wings? The engines’ position and size also looked fishy to me, quite small/narrow and very far high and back – I had doubts concerning the center of gravity. Nevertheless, I liked the idea, and the idea of an “A-10-esque remix” of the classic Frogfoot was born.

 

This idea was fueled even further when I found out that the Hobbycraft kit lends itself to such a conversion. The kit itself is not a brilliant Su-25 rendition, there are certainly better models of the aircraft in 1:72. However, what spoke for the kit as whiffing fodder was/is the fact that it is quite cheap (righteously so!) and AFAIK the only offering that comes with separate engine nacelles. These are attached to a completely independent central fuselage, and this avoids massive bodywork that would be necessary (if possible at all) with more conventional kits of this aircraft.

Another beneficial design feature is that the wing roots are an integral part of the original engine nacelles, forming their top side up to the fuselage spine. Through this, the original wingspan could be retained even without the nacelles, no wing extension would be necessary to retain the original proportions.

 

Work started with the central fuselage and the cockpit tub, which received a different (better) armored ejection seat and a pilot figure; the canopy remained unmodified and closed, because representing the model with an open cockpit would have required additional major body work on the spinal area behind the canopy. Inside, a new dashboard (from an Italeri BAe Hawk) was added, too – the original instrument panel is just a flat front bulkhead, there’s no space for the pilot to place the legs underneath the dashboard!

 

In parallel, the fin underwent major surgery. I initially considered an A-10-ish twin tail, but the Su-25’s high “tail stinger” prevented its implementation: the jet efflux would come very close to the tail surfaces. So, I went for something similar to the “Su-125” layout.

Mounting the OOB stabilizers to the fin was challenging, though. The fin lost its di-electric tip fairing, and it was cut into two sections, so that the tip would become long enough to match the stabilizers. A lucky find in the scrap box was a leftover tail tip from a Matchbox Blackburn Buccaneer, already shortened from a former, stillborn project: it had now the perfect length to take the Su-25 stabilizers! To make it fit on the fin, an 8mm deep section was inserted, in the form of a simple 1.5mm styrene sheet strip. Once dry, the surface was re-built with several PSR layers. Since it would sit further back on the new aircraft’s tail, the stinger with a RHAWS sensor was shortened.

 

On the fuselage, the attachment points for the wings and the engine nacelles were PSRed away and the front section filled with lots of lead beads, hoping that it would be enough to keep the model’s nose down.

 

Even though the wings had a proper span for a re-location into a low position, they still needed some attention: at the roots, there’s a ~1cm wide section without sweep (the area which would normally cover the original engine nacelles’ tops). This was mended through triangular 1.5 mm styrene wedges that extended the leading-edge sweep, roughly cut into shape once attached and later PSRed into the wings’ surfaces

 

The next construction site were the new landing gear attachment points. This had caused some serious headaches – where do you place and stow it? With new, low wings settled, the wings were the only logical place. But the wings were too thin to suitably take the retracted wheels, and, following the idea of a retrofitted existing design, I decided to adopt the A-10’s solution of nacelles into which the landing gear retracts forward, with the wheels still partly showing. This layout option appears quite plausible, since it would be a “graft-on” solution, and it also has the benefit of leaving lots of space for underwing stores, since the hardpoints’ position had to be modified now, too.

I was lucky to have a pair of A-10 landing gear nacelles at hand, left over from a wrecked Matchbox model from childhood time (the parts are probably 35 years old!). They were simply cut out, glued to the Su-25 wings and PSRed into shape. The result looked really good!

 

At this point I had to decide the model’s overall layout – where to place the wings, the tail and the new engine nacelles. The latter were not 1:72 A-10 transplants. I had some spare engine pods from the aforementioned Matchbox wreck, but these looked too rough and toylike for my taste. They were furthermore too bulky for the Su-25, which is markedly smaller than an A-10, so I had to look elsewhere. As a neat alternative for this project, I had already procured many moons ago a set of 1:144 resin PS-90A engines from a Russian company called “A.M.U.R. Reaver”, originally intended for a Tu-204 airliner or an Il-76 transport aircraft. These turbofan nacelles not only look very much like A-10 nacelles, just a bit smaller and more elegant, they are among the best resin aftermarket parts I have ever encountered: almost no flash, crisp molding, no bubbles, and perfect fit of the parts – WOW!

With these three elements at hand I was able to define the wings’ position, based on the tail, and from that the nacelles’ location, relative to the wings and the fin.

 

The next challenge: how to attach the new engines to the fuselage? The PS-90A engines came without pylons, so I had to improvise. I eventually found suitable pylons in the form of parts from F-14A underwing missile pylons, left over from an Italeri kit. Some major tailoring was necessary to find a proper position on the nacelles and on the fuselage, and PSRing these parts turned out to be quite difficult because of the tight and labyrinthine space.

 

When the engines were in place, work shifted towards the model’s underside. The landing gear was fully replaced. I initially wanted to retain the front wheel leg and the main wheels but found that the low wings would not allow a good ground clearance for underwing stores and re-arming the aircraft, a slightly taller solution was necessary. I eventually found a complete landing gear set in the scrap box, even though I am not certain to which aircraft it once belonged? I guess that the front wheel came from a Hasegawa RA-5C Vigilante, while the main gear and the wheels once belonged to an Italeri F-14A, alle struts were slightly shortened. The resulting stance is still a bit stalky, but an A-10 is also quite tall – this is just not so obvious because of the aircraft’s sheer size.

 

Due to the low wings and the landing gear pods, the Su-25’s hardpoints had to be re-arranged, and this eventually led to a layout very similar to the A-10. I gave the aircraft a pair of pylons inside of the pods, plus three hardpoints under the fuselage, even though all of these would only be used when slim ordnance was carried. I just fitted the outer pair. Outside of the landing gear fairings there would have been enough space for the Frogfoot’s original four outer for pylons, but I found this to be a little too much. So I gave it “just” three, with more space between them.

The respective ordnance is a mix for a CAS mission with dedicated and occasional targets. It consists of:

- Drop tanks under the inner wings (left over from a Bilek Su-17/22 kit)

- A pair of B-8M1 FFAR pods under the fuselage (from a vintage Mastercraft USSR weapon set)

- Two MERs with four 200 kg bombs each, mounted on the pylons outside of the landing gear (the odd MERs came from a Special Hobby IDF SMB-2 Super Mystère kit, the bombs are actually 1:100 USAF 750 lb bombs from a Tamiya F-105 Thunderchief in that scale)

- Four CBU-100 Rockeye Mk. II cluster bombs on the outer stations (from two Italeri USA/NATO weapon sets, each only offers a pair of these)

Yes, it’s a mix of Russian and NATO ordnance – but, like the real Georgian Su-25KM “Scorpion” upgrade, the TAM-1 would certainly be able to carry the same or even a wider mix, thanks to modified bomb racks and wirings. Esp. “dumb” weapons, which do not call for special targeting and guidance avionics, are qualified.

The gun under the nose was replaced with a piece from a hollow steel needle.

  

Painting and markings:

Nothing unusual here. I considered some more “exotic” options, but eventually settled for a “conservative” Soviet/Russian-style four-tone tactical camouflage, something that “normal” Su-25s would carry, too.

The disruptive pattern was adapted from a Macedonian Frogfoot but underwent some changes due to the T-tail and the engine nacelles. The basic tones were Humbrol 119 (RAF Light Earth), 150 (Forest Green), 195 (Chrome Oxide Green, RAL 6020) and 98 (Chocolate) on the upper surfaces and RLM78 from (Modelmaster #2087) from below, with a relatively low waterline, due to the low-set wings.

As usual, the model received a light black ink washing and some post-shading – especially on the hull and on the fin, where many details had either disappeared under PSR or were simply not there at all.

 

The landing gear and the lower areas of the cockpit were painted in light grey (Humbrol 64), while the upper cockpit sections were painted with bright turquoise (Modelmaster #2135). The wheel hubs were painted in bright green (Humbrol 101), while some di-electric fairings received a slightly less intense tone (Humbrol 2). A few of these flat fairings on the hull were furthermore created with green decal sheet material (from TL Modellbau) to avoid masking and corrections with paint.

 

The tactical markings became minimal, matching the look of late Georgian Su-25s. The roundels came from a Balkan Models Frogfoot sheet. The “07” was taken from a Blue Rider decal sheet, it actually belongs to a Lithuanian An-2. Some white stencils from generic MiG-21 and Mi-8 Begemot sheets were added, too, and some small markings were just painted onto the hull with yellow.

 

Some soot stains around the jet nozzles and the gun were added with graphite, and finally the kit was sealed with a coat of matt acrylic varnish.

  

A major bodywork project – and it’s weird that this is basically just a conversion of a stock kit and no kitbashing. A true Frogfoot remix! The new engines were the biggest “outsourced” addition, the A-10 landing gear fairings were a lucky find in the scrap box, and the rest is quite generic and could have looked differently. The result is impressive and balanced, though, the fictional TAM-1 looks quite plausible. The landing gear turned out to be a bit tall and stalky, though, making the aircraft look smaller on the ground than it actually is – but I left it that way.

If anyone can do it, you can .

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I found this on the sidewalk, in this condition, about a mile from my residence . So far as i know and recall, every flier i have from this past election with a Democratic Party candidate's photo on it and urging me to vote for the person, i found on the ground ; and any which may have been directed to my mailbox either did not make it or were filched by lock-picking memorabilia collectors . On the other hand, 6 pro-Trump fliers did make it to my mailbox .

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I believe that it is possible for people of public trust to betray their trust ; in matters small, and matters consequential .

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An open letter,

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Mister President Obama, Mister Secretary Kerry, come to Allentown . This is your point of contact, or it should be .

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Come and help motivate us to gather together in self-caucus to find out if what has been claimed in the return regarding our vote, (cast largely upon DRE machines without VVPAT), resembles the way we collectively recall voting . Come and help set aside futility which lies upon us --- not just about this past election --- but for all future ones ... for i can tell you there are some on the street who will publically say what you will not, "I think it was rigged" . Come and encourage us to forgive all who will publically say how we cast our vote, for whomever it may have been, from whomever it may have come . Come encourage us to to risk retribution by opposing publically and, may it be so, effectively one not famous for a forgiving nature .

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There is a gulf opening on the street, between the tribes, the colors --- and you are feeding our despair by taking an untrusted and untested result as final . You look a coward smiling at people whose deeds you should oppose, if you do not ; and showing love to one whose elevation you should question, and have not . You are letting us down ; and i believe that if this mood on the street finds its own outlet, as it inevitably must --- if it is not directed toward the effective to alloy the love you feel guided to show even Mr. Donald Trump --- people will be hurt . That may include me .

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Be daring, Mr. President . Brave the show trial the Republicans may put you through for your efforts . Brave impeachment and conviction and prison and even a death-sentence to reveal to the people of this country and this world that you have you own conviction . That you have The conviction . We are living in, "the fierce urgency of now", now ; and it is time for you to own your rhetoric .

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If fraud exists in our election industry, and if it is as broad and deep and persistant and as favorable to the right as i believe it may be, another 2 or 4 or 8 years would only be our ticket deeper into oblivion . With a chance to fortify their position with Supreme Court and Service Commandant appointments --- solely of their own choosing --- the right wing of the Republican Party may put the Democratic Party itself on show trial if it ever again rises to the level of challenge .

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Come also to listen to our clergy and our barbers, the latter especially ; for while a good Reverend rises to speak, a good barber rises to listen . The Democratic Party needs a farm system as badly as, (i believe), it needs honest elections . It needs local talent to bring local voters to the polls in off and off-off year elections . These people can put you in touch with those whom, though they may not have resources or a spotless record, can make up for this with aptitude and interest and the neighborhood credibility to make a strong run ; and serve well in office .

.

The chance we can do these things without you is very small .

.

.

.

Below are some items that i hope will be helpful and challenging to you ; (including some redundancy) .

.

.

.

The following is edited and expanded from a response i made on my facebook timeline, (michaelcharlesyoung), to a post by 350, (dot org) .

{

Please also see my timeline's previous posts on the matter : 09 November, 18 October, 03 August, and 09 June 2016 . Thank you .

}

.

One approach to fighting a Trump administration's likely effects on global warming might be to contest the results .

.

This could be attempted by helping voters in counties, (where DRE, {direct-recording electronic}, voting machines, {without Voter Verified Paper Audit Trail, VVPAT} were being used), (in states which went unexpectedly, or unexpectedly strongly, to Trump on election day), self-caucus to determine who it was we recall having voted for . If the such caucuses can be made sufficiently complete, and if they show results broadly different than those presented in the official return, participating voters could be asked to confirm our recollections with signed affidavits which could form the basis of class-action lawsuits challenging the returns ; (and the trade-secrecy protection of computerized voting machines’ software and hardware) . If sufficiently broad differences can be found, i believe a suit could be brought challenging the result itself .

.

{

Here i note that each DRE machine, so far as i recall having been told, is put through a "logic and accuracy test" immediately prior to the opening of each polling place .

.

As i recall, this involves a polling place worker booting the machine, and either during the boot process with instructions to the Basic Input-Output System, (BIOS), or following the loading of the Operating System, (OS), setting the system clock to an hour during which the election would be in progress . The worker then pretends to be a series of voters, casting ballots which would cover all voting options . The worker then verifies that these options have been faithfully recorded ; and if so, would clear or otherwise remove these test votes . The machine would then be rebooted for use in the election, with the system clock returned to the current time . It is important to note that the polling place worker would be acting in good faith here .

.

However, i have enough experience programming computers to believe that with sufficient skills, ingenuity, tools and access, the computerized voting machine can be programmed to pass such test --- whether or not it is also programmed to be accurate or even honest during the election . Regarding this matter, i feel that Wikipedia's page on a bundle of software called a Rootkit may have relevant information .

.

In (the at least imagined) light of the above, i believe that if broad discrepancies between the above-suggested self-caucusing and the official returns were to be found, a suit could be brought against the election result itself ... as it would mean that misrepresentation of the vote is/was either on the part of a great many self-revealed and sworn voters, or, intentionally, on the part of some skillful person or persons who had accessed and programmed, (or reprogrammed), the machines .

.

I stress that i do not consider sworn self-declaration by voters to be a "recount" of an election, but a "real" count, (should sufficient numbers of voters participate) . In my opinion, should broad discrepancies implying that anyone's vote had been undercounted, (within the computerized voting equipment), be found between the sworn, self-declared vote and the, (largely machine generated), return, the two most likely explanations would be that either

:

1) Many people who trustingly, (or grudgingly), cast ballots upon these DRE machines, (without VVPAT), would be lying in their subsequent affidavits regarding how they had voted .

Or that

:

2) The machines would have been maliciously and skillfully programmed (or reprogrammed) to lie on the record, seamlessly and invisibly ; and to do so after passing a logic and accuracy test run by polling place workers acting in good faith . In such a case, there would never have been a count of the vote to begin with, only the pretense of a count .

.

I note also that i believe criminal conspiracies have a tendency to leak in direct proportion to the number of people involved . Thus i believe that if election fraud is being conducted within the computerized voting equipment, the polling place workers themselves would probably be kept in the dark about it ; though they might be aware of irregularities such as, (hypothetically), not posting a polling place's unofficial return in the window following the election, (should this be required), for whatever duration of time this might be required .

}

.

If it can be brought to this point, i hope that Rev. Dr. Martin Luther King Jr. style demonstrations --- well dressed, well mannered, determined people exercising our right to peaceably assemble and to petition our government --- you, President Barack Obama, specifically --- for a redress of grievances, will prompt you to put our suit before the Supreme Court .

.

I live in Allentown, (Lehigh County), Pennsylvania ; where our polling places use DRE machines, (without VVPAT), (provided by Diebold) . According to the best information i have, our county delivered some 50-60% of our vote to Hillary Clinton . That seems low to me, and i have been trying to encourage the people of Allentown to self-caucus . The help of your organization and your followers would be appreciated .

.

Our neighboring county, Northampton, is said to have delivered a plurality of its vote to Donald Trump . This may also be worth checking by means of self-caucus .

.

Several counties, (including Miami-Dade), in Florida may likewise be worth the effort .

.

In the hypothetical case that both Pennsylvania and Florida were stolen for Donald Trump by means of skillful fraud on the part of people who had programmed DRE machines without VVPAT, the wrong person would now be President-elect .

.

Time seems quite short, though . I feel that protest by itself will not salvage the situation ; that demonstration had best be behind something with legal merit, (as i feel this would have) ; something which --- if you, President Obama, have the courage --- could forwarded directly to the Supreme Court .

.

If, as seems likely, the Supreme Court deadlocks, i feel that the you, as President, have the authority to convene a Court Martial --- comprised of the Joint Chiefs of Staff, and of each service’s Chief Legal Officer, and of each service's Chief Information Technology Officer, plus two randomly chosen, (from among those willing and still in the service), Congressional Medal of Honor winners --- to attempt likewise to reach a ruling . This would be because our nation’s military oaths of office state first, (and presumably foremost), an obligation to support and defend the constitution of the United States against all enemies, foreign and domestic ; and secondly, for enlisted personnel, an obligation to obey the orders of the President of the United States, (the officer's like duty is implicit in the President's role as Commander in Chief) . Thus i feel that the military, to have a clear obligation of duty, is entitled, should the Supreme Court deadlock and the President convene Court Martial upon the matter, to issue a binding ruling .

.

I would take this logic farther . As i see it, Article Two of the U.S. Constitution gives the President, (as Commander in Chief), no authority to require the military to accept transfer of power to a person whose fitness for command, or the legitimacy of whose election, or both, is seriously in doubt . In such case, i believe that the Joint Chiefs would have the right to convene Court Martial proceedings upon the matter over and above any order or measure to the contrary .

.

Please also get in touch with verifiedvoting, (dot org), where they have maps of the counties withing Pennsylvania and Florida using DRE machines without VVPAT .

+++ 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.

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

 

+++ 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.

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+++ 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 North American A-5 Vigilante (Prior to 1962 unification of Navy and Air Force designations, it was designated the A3J) was an American carrier-based supersonic bomber designed and built by North American Aviation for the United States Navy. In 1953, North American Aviation began a private study for a carrier-based, long-range, all-weather strike bomber, capable of delivering nuclear weapons at supersonic speeds. This proposal, the North American General Purpose Attack Weapon (NAGPAW) concept, was accepted by the United States Navy, with some revisions, in 1955. A contract was awarded on 29 August 1956. Its first flight occurred two years later, on 31 August 1958 in Columbus, Ohio.

 

At the time of its introduction, the Vigilante was one of the largest and by far the most complex aircraft to operate from a Navy aircraft carrier. It had a high-mounted swept wing with a boundary-layer control system (blown flaps) to improve low-speed lift. It had no ailerons; roll control was provided by spoilers in conjunction with differential deflection of the all-moving tail surfaces. The use of aluminum-lithium alloy for wing skins and titanium for critical structures was also unusual. The A-5 had two widely spaced General Electric J79 turbojet engines, fed by inlets with variable intake ramps, and a single large all-moving vertical stabilizer. Preliminary design studies employed twin vertical fin/rudders, but this was eventually changed to a single tall but foldable fin. The wings and the nose radome folded for carrier stowage, too. The Vigilante had a crew of two seated in tandem, a pilot and a bombardier-navigator (BN) (reconnaissance/attack navigator (RAN) on later reconnaissance versions).

 

The Vigilante had advanced and complex electronics when it first entered service. It had one of the first "fly-by-wire" systems on an operational aircraft (with mechanical/hydraulic backup) and a computerized AN/ASB-12 nav/attack system incorporating a head-up display ("Pilot's Projected Display Indicator" (PPDI), one of the first), multi-mode radar, radar-equipped inertial navigation system (REINS, based on technologies developed for North American's Navaho missile), closed-circuit television camera under the nose, and an early digital computer known as "Versatile Digital Analyzer" (VERDAN) to run it all.

 

The aircraft replaced the subsonic Douglas A-3 Skywarrior as the Navy's primary nuclear-strike aircraft, but only briefly. Given its original design as a carrier-based, supersonic, nuclear heavy attack aircraft, the Vigilante’s main armament was carried in an unusual internal "linear bomb bay" between the engines in the rear fuselage, which allowed the bomb to be dropped at supersonic speeds. The single nuclear weapon, commonly the Mk 28 bomb, was attached to two disposable fuel tanks in the cylindrical bay in an assembly known as the "stores train". A set of extendable fins was attached to the aft end of the most rearward fuel tank. These fuel tanks were to be emptied during the flight to the target and then jettisoned with the bomb by an explosive drogue gun. The stores train was propelled rearward at about 50 feet (15 m) per second (30 knots) relative to the aircraft. It then followed a ballistic path.

 

The Vigilante originally had two wing pylons, intended primarily for drop tanks. The second Vigilante variant, the A3J-2 (A-5B), incorporated internal tanks for an additional 460 gallons of fuel, which added a pronounced dorsal "hump", along with two additional wing hardpoints, for a total of four. Other improvements included blown flaps on the leading edge of the wing, changes to the air intakes and stronger landing gear.

 

The reconnaissance version of the Vigilante, the RA-5C, was based on the A-5B airframe and had slightly greater wing area and added a long canoe-shaped fairing under the fuselage for a multi-sensor reconnaissance pack. This added an APD-7 side-looking airborne radar (SLAR), AAS-21 infrared line scanner, and camera packs, as well as improved electronic countermeasures. An AN/ALQ-61 electronic intelligence system could also be carried. The RA-5C retained the AN/ASB-12 bombing system, and could, in theory, carry weapons, although it never did in service. Later-built RA-5Cs had more powerful J79-10 engines with afterburning thrust of 17,900 lbf (80 kN), the same engines as the Navy’s F-4J Phantom IIs. The reconnaissance Vigilante weighed almost five tons more than the strike version with almost the same thrust and an only modestly enlarged wing. These changes reduced its acceleration and climb rate, though it remained fast in level flight and was still fully carrier-capable.

 

The last Vigilante version to be developed from 1964 on and to enter service in 1966 was the EA-5D, a dedicated electronic reconnaissance and electronic warfare version, again replacing respective A-3 Skywarrior variants. With the initial experience from the Vietnam conflict, the EA-5D was primarily conceived as a fast escort for supersonic strike aircraft – namely the USN’s F-4 Phantom IIs which progressively took over more strike missions and direly needed protection from SAMs that could keep up with them during their dangerous missions over enemy territory.

 

The EA-5D, which was unofficially nicknamed “Electric Vigilante”, “Eva” or simply “E-V” by its crews, was based on the late RA-5C’s airframe and was easily distinguishable through its fairing at the top of the fin which contained the electronics for a Bunker-Ramo AN/ALQ-86 ECM suite. It carried ECM gear in the linear bomb bay and a 16 feet (4.9 m) long canoe-shaped ventral fairing (looking like a shortened but deeper version of the RA-5C’s camera and SLAR installation), plus a heat exchanger, a non-jettisonable auxiliary tank and AN/ALE-41 chaff dispensers in an extended tail cone. The complete installation weighed some 6,000 pounds (2,700 kg). Receivers were installed in a fin-tip pod, or "football", like that of the contemporary EA-6A. This fin array caused some lateral instability, though, which could be compensated with a pair of fins under the rear fuselage.

 

Like the RA-5C, the EA-5D retained the AN/ASB-12 bombing system and was – in theory – like its recce sibling capable to carry out strike missions, but this never happened either. The EA-5Ds were furthermore equipped with an AN/APQ-129 fire control radar, making the aircraft capable of SEAD missions and of firing the AGM-45 “Shrike” anti-radiation missile, although they were apparently never used in that offensive role. Up to four ram-air turbine powered ALQ-76 countermeasures pods could be carried on the underwing hardpoints, augmenting the internal AN/ALQ-86 system’s bandwidth and jamming power. To improve survivability the EA-5D was furthermore outfitted with a pair of launch rails, mounted as sub-pylons on the outsides of the outer underwing hardpoints. Each could carry a single IR-guided AIM-9 Sidewinder AAM.

 

Despite the Vigilante's useful service as reconnaissance and ECM platform, it was expensive and complex to operate and occupied significant amounts of precious flight and hangar deck space aboard both conventional and nuclear-powered aircraft carriers at a time when carrier air wings, with the introduction of the F-14 Tomcat and S-3 Viking, were averaging 90 aircraft, many of which were larger than their predecessors. Moreover, the Vigilante did not end the career of the A-3 Skywarrior, which would carry on as photo reconnaissance aircraft, electronic warfare platforms, aerial refueling tankers, and executive transport aircraft designated as RA-3A/B, EA-3A/B, ERA-3B, EKA-3B, KA-3B, and VA-3B, into the early 1990s.

 

Only 28 EA-5Ds were built (two prototypes, 15 new-build, and 11 conversions from existing A-5A and RA-5C airframes) and the United States remained the only operator of the type. The EA-5D saw extensive use in Vietnam and seven machines were lost (four to SAMs, one to a VPAF MiG-21 and two through accidents), but after the end of hostilities and massive reductions of military expenses the EA-5D was quickly phased out from frontline service in the late 1970s, after an active career of just twelve years. In service it was replaced by the subsonic but much more potent EA-6B “Prowler”, which was based on the carrier-capable A-6 “Intruder” bomber, primarily to reduce the number of types in the USN’s arsenal and therewith operating costs and complexity. Since the EA-6B offered much higher ECM capabilities, the small EA-5D fleet was never upgraded, e. g. with the 2nd generation AGM-78 “Standard” ARM or the AN/ALQ-99 ECM pods.

 

However, a handful of “Electric Vigilantes” remained active with VAQ-137 (“Rooks”) until the late Eighties – long enough to receive the USN’s new tactical low-visibility paint scheme. These EA-5Ds were operated from land-bases only, not assigned to a Carrier Air Group, with a dedicated tail code (“KW”) to reflect this special status. They acted primarily as electronic aggressor aircraft but were also used to simulate supersonic cruise missiles like the contemporary Soviet Kh-20 (AS-3 “Kangaroo”) or Kh-22 (AS-4 “Kennel”) against land and sea targets during training and naval NATO maneuvers. Thanks to their size, speed and flight characteristics the aircraft were also employed as supersonic bomber aggressors, mimicking Soviet Tu-22s or Su-24s. Most of the Evas therefore received more or less authentic temporary Red Star decorations on their fins, which were, however, rarely overpainted after training missions and became part of the “standard markings”.

In 1987 the machines were finally retired, their airframes had reached their structural limit and maintenance costs of the complex aircraft had become prohibitive. They were in the electronic aggressor role eventually replaced with subsonic and much more economical EA-7L Corsair IIs.

  

General characteristics:

Crew: 2

Length: 76 ft 6 in (23.32 m)

Wingspan: 53 ft 0 in (16.16 m)

Height: 19 ft 5 in (5.91 m)

Wing area: 701 sq ft (65.1 m)

Empty weight: 32,783 lb (14,870 kg)

Gross weight: 47,631 lb (21,605 kg)

Max takeoff weight: 63,085 lb (28,615 kg)

Fuel capacity: 2,805 US gal (10,618 L; 2,336 imp gal) internal

or 19,074 lb (8,652 kg) of JP-5,

or 24,514 lb (11,119 kg) with 2 × 400 US gal external tanks

 

Powerplant:

2× General Electric J79-GE-10 after-burning turbojet engines,

10,900 lbf (48 kN) thrust each dry, 17,900 lbf (80 kN) with afterburner

 

Performance:

Maximum speed: 1,322 mph (Mach 2, 1,149 kn, 2,128 km/h) at 40,000 ft (12,000 m)

Combat range: 974 nmi (1,121 mi, 1,804 km)

Ferry range: 1,571 nmi (1,808 mi, 2,909 km)

Service ceiling: 52,100 ft (15,900 m)

g limits: +5

Rate of climb: 33,900 ft/min (172 m/s)

Wing loading: 80.4 lb/sq ft (393 kg/m2)

Thrust/weight: 0.72

 

Armament:

4x underwings pylons, each with a load capability of up to 2.000 lb (950 kg),

typically occupied with 400 US gal drop tanks or ALQ-76 Tactical Jamming System (TJS)

ECM pods. Other potential loads: AN/ALE-43(V)1&4 Bulk Chaff Dispensing System pod,

a single AN/AAQ-28(V) Litening targeting pod or AGM-45 Shrike anti-radar missiles

2x launch rails for defensive AIM-9 Sidewinder AAMs on the outer pylons

  

The kit and its assembly:

This what-if project had been lingering for a long time in the back of my mind, and I shoved it a side for years because of the model’s sheer size that eats up a lot of display space – even though I had the hardware already stashed away, collecting dust. While the build was rather inspired by its livery (see below) I wondered why the Vigilante, an elegant and impressive aircraft, had not been adapted to the ECM role? The concept of a supersonic penetrator/protector aircraft was realized by the USAF with the EF-111A Raven, but in the Vigilante’s time frame, the Vietnam War, esp. its end phase, an escort for fast USN attack aircraft might have made sense, so that I tried to mate the RA-5C with contemporary ECM technology and typical details – and the result became the fictional EA-5D.

 

With this idea the model became only a conversion of a basic airframe, not a spectacular kitbashing. Since I knew the Hasegawa RA-5C and its underwhelming quality/detail, I settled for the Trumpeter kit – a MUCH better but also a bit über-complicated offering. It is, however, better in any respect, even though you can ask why the cockpit has to consist of no less than thirty (!) parts (including seats and dashboard films), and the pylons as well as even the thin stabilizers and the fin have to consist of halves? One can also wonder why the kit comes with four(!) free-fall nukes but none of the RA-5C’s typical 400 gallon drop tanks? The kit features the type’s underwing flare dispensers, though. If there is something to criticize it’s the lack of air intake ducts – behind the wedge-shaped intakes and their ramps there is nothing inside the fuselage. Since I did not want to put too much effort into that flaw I simple blocked sight into the model’s body with a bulkhead made from black foamed styrene.

Everything goes together quite well, except for the fuselage halves which appear somewhat warped, and the rather massive plastic makes work easy. Despite this splendor of material, the sandwich leading and trailing edges are surprisingly thin and look pretty good.

 

While the RA-5C was at its core built OOB there were – naturally – some external mods to convey its ECM role. Most obvious detail is the fin top fairing, procured from a KiTech EA-6B, a shabby copy of the Hasegawa kit. This also provided the ECM pods and the pair of voluminous drop tanks.

The retrofitted Sidewinder launch rails on the outer pylons came from an Emhar FJ-4B, the then-state-of-the-art all-aspect AIM-9Ls came from a Hasegawa F-4 kit. To emphasize its electronic mission I added some antenna fairings around the hull. Beyond the fin pod, the EA-5D received sensor fairings along the flanks, inspired by the USAF F-105Gs’arrangement along the bomb bay, a shallow dorsal bulge behind the cockpits and some blister and blade antennae all around the hull.

 

The large ventral fairing that replaced the RA-5C’s “camera canoe” was scratched from a drop tank half, from a chunky Kangnam MiG-31, in an attempt to create something that the reminds of the EF-111’s arrangement. A ventral adapter for a display holder was integrated into the hull, too, for in-flight scenes.

A pair of long stabilizer fins was added under the rear fuselage, too, because I think that the large tail fin pod could somewhat hamper directional stability… The consist of rotor blades from a Matchbox SA.360 Dauphin helicopter.

The Vigilante’s tail cone, the former fairing for the linear bomb bay between the engines, was also heavily modified, with a thimble-shaped radome and a separate fairing for an internal chaff dispenser underneath, for a different look. To make the model look a bit more lively, esp. in its all-grey low-viz livery (see below) I mounted the flaps (all six are separate elements, and the inner pairs consist of lower and upper halves, too!) in lowered position.

  

Painting and markings:

The original reason to build this whiffy Vigilante was to see how the sleek and elegant aircraft would look in early USN low-viz colors! With this idea in mind the scheme was improvised and very simple: FS 36320 on the upper surfaces and FS 36375 underneath (Humbrol 128 and 127, respectively), on the flanks (with a relatively high waterline) and the fin. A slightly darker blue grey (FS 35237, Humbrol 145) was used for an anti-glare panel in front of the windshield. Most di-electric panels and the nose radome were painted in brownish light grey (RAL 7032, Revell 75), for low contrast but a significantly different color.

 

Inside, the landing gear as well as the air intakes were painted gloss white, the cockpit was painted in neutral grey (FS 36231) with dark grey ejection seats. The latter appears a bit tone-in-tone with the all-grey outside, but that was apparently the A-5’s interior design in real life.

 

To add some variety to the grey livery I painted the ordnance in “old” USN colors: the drop tanks became all-white and the ECM pods also received a white base. The AIM-9Ls on the extra launch rails (also painted white) received blue bodies as training missiles, with black seeker heads and white tail fins.

The wings’ leading edges (bare steel?) were masked and then painted with Revell 91 (iron metallic).

 

The whole model received a washing with thinned black ink to emphasize the many recessed rivets and panel lines, and then I added panel counter shading with lighter basic tones, also trying to create a slightly worn/weathered and not-so-uniform finish on the large grey surfaces, which underline the Vigilante’s elegant lines but also look quite boring, due to the sheer size/area, esp. from above.

 

The low-viz markings were improvised and puzzled together from various sources. The Red Stars on the fin were inspired by real-world aggressor markings, AFAIK some A-7Ls, EA-3Bs and A-4Fs carried such decorations, even paired with large bort numbers on the nose.

To improve the worn/grimy look I also treated the model’s surfaces with grinded graphite – only lightly, but I wanted to make the large grey areas to look even more diverse than just with the initial paint effects.

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

 

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.

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.

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?"

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/

 

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.

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.

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

 

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

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).

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."

 

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

 

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?"

I've gone back and forth so many times on how I want this quilt to turn out! I decided that I'll ask the group to make wonky stars. I'll send each person 9 different fabrics and a lot of backing fabric so they can have the option to make 1 (or many) blocks in any combination of 3,6 or 12 inches. Whew!

Framed by a perfect blue sky and a symmetrical arc of neoclassical stone, the Military Women’s Memorial stands as a solemn tribute to the more than three million women who have served in the United States Armed Forces. Located at the ceremonial entrance to Arlington National Cemetery in Washington D.C., this photo captures the serene yet powerful facade of the nation’s only major national memorial honoring women’s contributions to the military across all branches and eras.

 

Designed by architects Marion Weiss and Michael Manfredi, the structure—officially called the Women In Military Service For America Memorial—was completed in 1997 and integrates seamlessly into the historic landscape. It was built into the existing Hemicycle, an imposing semicircular retaining wall originally intended as part of a ceremonial gateway but left unused since the 1930s. In this view, the monumental granite arch commands attention at the center, framed by clean lines, open walkways, and elegant balustrades.

 

The memorial is more than architectural splendor; it functions as a museum, archive, and gathering place. Inside, visitors can explore exhibitions, personal stories, and artifacts that illuminate the complex and often underrepresented history of women in uniform—from Revolutionary War heroes disguised as men to contemporary combat commanders. At the heart of the interior is a computerized Register, cataloging the service records of women who have worn the nation’s uniform, preserving their legacies for future generations.

 

This photograph, taken in daylight under ideal conditions, emphasizes the clarity of the structure’s lines and the harmony between human design and natural surroundings. Leafless trees on the horizon echo the memorial's stark dignity, while the circular plaza in the foreground invites contemplation.

 

Located just across Memorial Avenue from the iconic Arlington Cemetery Welcome Center, the memorial is an essential stop for any visitor wishing to understand the full scope of American military service. It’s a space for quiet reflection, formal ceremonies, and education—especially on Veterans Day, Memorial Day, and during events celebrating Women’s History Month.

 

The Military Women’s Memorial stands as a crucial corrective to the historical erasure of women’s service. It tells a broader American story—of duty, perseverance, and change—etched in stone and carried forward through storytelling. This image captures the physical and symbolic gateway to that narrative, as timeless and resilient as the women it honors.

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.

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.

 

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).

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

  

From Wikipedia, the free encyclopedia

 

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

 

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

 

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

 

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

 

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

 

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

 

Development

 

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

 

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

 

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

  

Design

 

Overview

 

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

 

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

 

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

  

Improvements

 

Ostensible improvements over past-generation fighter aircraft include:

 

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

 

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

 

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

 

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

 

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

 

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

 

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

 

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

  

Costs

 

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

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.

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?"

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.

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.

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.

+++ 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 North American A-5 Vigilante (Prior to 1962 unification of Navy and Air Force designations, it was designated the A3J) was an American carrier-based supersonic bomber designed and built by North American Aviation for the United States Navy. In 1953, North American Aviation began a private study for a carrier-based, long-range, all-weather strike bomber, capable of delivering nuclear weapons at supersonic speeds. This proposal, the North American General Purpose Attack Weapon (NAGPAW) concept, was accepted by the United States Navy, with some revisions, in 1955. A contract was awarded on 29 August 1956. Its first flight occurred two years later, on 31 August 1958 in Columbus, Ohio.

 

At the time of its introduction, the Vigilante was one of the largest and by far the most complex aircraft to operate from a Navy aircraft carrier. It had a high-mounted swept wing with a boundary-layer control system (blown flaps) to improve low-speed lift. It had no ailerons; roll control was provided by spoilers in conjunction with differential deflection of the all-moving tail surfaces. The use of aluminum-lithium alloy for wing skins and titanium for critical structures was also unusual. The A-5 had two widely spaced General Electric J79 turbojet engines, fed by inlets with variable intake ramps, and a single large all-moving vertical stabilizer. Preliminary design studies employed twin vertical fin/rudders, but this was eventually changed to a single tall but foldable fin. The wings and the nose radome folded for carrier stowage, too. The Vigilante had a crew of two seated in tandem, a pilot and a bombardier-navigator (BN) (reconnaissance/attack navigator (RAN) on later reconnaissance versions).

 

The Vigilante had advanced and complex electronics when it first entered service. It had one of the first "fly-by-wire" systems on an operational aircraft (with mechanical/hydraulic backup) and a computerized AN/ASB-12 nav/attack system incorporating a head-up display ("Pilot's Projected Display Indicator" (PPDI), one of the first), multi-mode radar, radar-equipped inertial navigation system (REINS, based on technologies developed for North American's Navaho missile), closed-circuit television camera under the nose, and an early digital computer known as "Versatile Digital Analyzer" (VERDAN) to run it all.

 

The aircraft replaced the subsonic Douglas A-3 Skywarrior as the Navy's primary nuclear-strike aircraft, but only briefly. Given its original design as a carrier-based, supersonic, nuclear heavy attack aircraft, the Vigilante’s main armament was carried in an unusual internal "linear bomb bay" between the engines in the rear fuselage, which allowed the bomb to be dropped at supersonic speeds. The single nuclear weapon, commonly the Mk 28 bomb, was attached to two disposable fuel tanks in the cylindrical bay in an assembly known as the "stores train". A set of extendable fins was attached to the aft end of the most rearward fuel tank. These fuel tanks were to be emptied during the flight to the target and then jettisoned with the bomb by an explosive drogue gun. The stores train was propelled rearward at about 50 feet (15 m) per second (30 knots) relative to the aircraft. It then followed a ballistic path.

 

The Vigilante originally had two wing pylons, intended primarily for drop tanks. The second Vigilante variant, the A3J-2 (A-5B), incorporated internal tanks for an additional 460 gallons of fuel, which added a pronounced dorsal "hump", along with two additional wing hardpoints, for a total of four. Other improvements included blown flaps on the leading edge of the wing, changes to the air intakes and stronger landing gear.

 

The reconnaissance version of the Vigilante, the RA-5C, was based on the A-5B airframe and had slightly greater wing area and added a long canoe-shaped fairing under the fuselage for a multi-sensor reconnaissance pack. This added an APD-7 side-looking airborne radar (SLAR), AAS-21 infrared line scanner, and camera packs, as well as improved electronic countermeasures. An AN/ALQ-61 electronic intelligence system could also be carried. The RA-5C retained the AN/ASB-12 bombing system, and could, in theory, carry weapons, although it never did in service. Later-built RA-5Cs had more powerful J79-10 engines with afterburning thrust of 17,900 lbf (80 kN), the same engines as the Navy’s F-4J Phantom IIs. The reconnaissance Vigilante weighed almost five tons more than the strike version with almost the same thrust and an only modestly enlarged wing. These changes reduced its acceleration and climb rate, though it remained fast in level flight and was still fully carrier-capable.

 

The last Vigilante version to be developed from 1964 on and to enter service in 1966 was the EA-5D, a dedicated electronic reconnaissance and electronic warfare version, again replacing respective A-3 Skywarrior variants. With the initial experience from the Vietnam conflict, the EA-5D was primarily conceived as a fast escort for supersonic strike aircraft – namely the USN’s F-4 Phantom IIs which progressively took over more strike missions and direly needed protection from SAMs that could keep up with them during their dangerous missions over enemy territory.

 

The EA-5D, which was unofficially nicknamed “Electric Vigilante”, “Eva” or simply “E-V” by its crews, was based on the late RA-5C’s airframe and was easily distinguishable through its fairing at the top of the fin which contained the electronics for a Bunker-Ramo AN/ALQ-86 ECM suite. It carried ECM gear in the linear bomb bay and a 16 feet (4.9 m) long canoe-shaped ventral fairing (looking like a shortened but deeper version of the RA-5C’s camera and SLAR installation), plus a heat exchanger, a non-jettisonable auxiliary tank and AN/ALE-41 chaff dispensers in an extended tail cone. The complete installation weighed some 6,000 pounds (2,700 kg). Receivers were installed in a fin-tip pod, or "football", like that of the contemporary EA-6A. This fin array caused some lateral instability, though, which could be compensated with a pair of fins under the rear fuselage.

 

Like the RA-5C, the EA-5D retained the AN/ASB-12 bombing system and was – in theory – like its recce sibling capable to carry out strike missions, but this never happened either. The EA-5Ds were furthermore equipped with an AN/APQ-129 fire control radar, making the aircraft capable of SEAD missions and of firing the AGM-45 “Shrike” anti-radiation missile, although they were apparently never used in that offensive role. Up to four ram-air turbine powered ALQ-76 countermeasures pods could be carried on the underwing hardpoints, augmenting the internal AN/ALQ-86 system’s bandwidth and jamming power. To improve survivability the EA-5D was furthermore outfitted with a pair of launch rails, mounted as sub-pylons on the outsides of the outer underwing hardpoints. Each could carry a single IR-guided AIM-9 Sidewinder AAM.

 

Despite the Vigilante's useful service as reconnaissance and ECM platform, it was expensive and complex to operate and occupied significant amounts of precious flight and hangar deck space aboard both conventional and nuclear-powered aircraft carriers at a time when carrier air wings, with the introduction of the F-14 Tomcat and S-3 Viking, were averaging 90 aircraft, many of which were larger than their predecessors. Moreover, the Vigilante did not end the career of the A-3 Skywarrior, which would carry on as photo reconnaissance aircraft, electronic warfare platforms, aerial refueling tankers, and executive transport aircraft designated as RA-3A/B, EA-3A/B, ERA-3B, EKA-3B, KA-3B, and VA-3B, into the early 1990s.

 

Only 28 EA-5Ds were built (two prototypes, 15 new-build, and 11 conversions from existing A-5A and RA-5C airframes) and the United States remained the only operator of the type. The EA-5D saw extensive use in Vietnam and seven machines were lost (four to SAMs, one to a VPAF MiG-21 and two through accidents), but after the end of hostilities and massive reductions of military expenses the EA-5D was quickly phased out from frontline service in the late 1970s, after an active career of just twelve years. In service it was replaced by the subsonic but much more potent EA-6B “Prowler”, which was based on the carrier-capable A-6 “Intruder” bomber, primarily to reduce the number of types in the USN’s arsenal and therewith operating costs and complexity. Since the EA-6B offered much higher ECM capabilities, the small EA-5D fleet was never upgraded, e. g. with the 2nd generation AGM-78 “Standard” ARM or the AN/ALQ-99 ECM pods.

 

However, a handful of “Electric Vigilantes” remained active with VAQ-137 (“Rooks”) until the late Eighties – long enough to receive the USN’s new tactical low-visibility paint scheme. These EA-5Ds were operated from land-bases only, not assigned to a Carrier Air Group, with a dedicated tail code (“KW”) to reflect this special status. They acted primarily as electronic aggressor aircraft but were also used to simulate supersonic cruise missiles like the contemporary Soviet Kh-20 (AS-3 “Kangaroo”) or Kh-22 (AS-4 “Kennel”) against land and sea targets during training and naval NATO maneuvers. Thanks to their size, speed and flight characteristics the aircraft were also employed as supersonic bomber aggressors, mimicking Soviet Tu-22s or Su-24s. Most of the Evas therefore received more or less authentic temporary Red Star decorations on their fins, which were, however, rarely overpainted after training missions and became part of the “standard markings”.

In 1987 the machines were finally retired, their airframes had reached their structural limit and maintenance costs of the complex aircraft had become prohibitive. They were in the electronic aggressor role eventually replaced with subsonic and much more economical EA-7L Corsair IIs.

  

General characteristics:

Crew: 2

Length: 76 ft 6 in (23.32 m)

Wingspan: 53 ft 0 in (16.16 m)

Height: 19 ft 5 in (5.91 m)

Wing area: 701 sq ft (65.1 m)

Empty weight: 32,783 lb (14,870 kg)

Gross weight: 47,631 lb (21,605 kg)

Max takeoff weight: 63,085 lb (28,615 kg)

Fuel capacity: 2,805 US gal (10,618 L; 2,336 imp gal) internal

or 19,074 lb (8,652 kg) of JP-5,

or 24,514 lb (11,119 kg) with 2 × 400 US gal external tanks

 

Powerplant:

2× General Electric J79-GE-10 after-burning turbojet engines,

10,900 lbf (48 kN) thrust each dry, 17,900 lbf (80 kN) with afterburner

 

Performance:

Maximum speed: 1,322 mph (Mach 2, 1,149 kn, 2,128 km/h) at 40,000 ft (12,000 m)

Combat range: 974 nmi (1,121 mi, 1,804 km)

Ferry range: 1,571 nmi (1,808 mi, 2,909 km)

Service ceiling: 52,100 ft (15,900 m)

g limits: +5

Rate of climb: 33,900 ft/min (172 m/s)

Wing loading: 80.4 lb/sq ft (393 kg/m2)

Thrust/weight: 0.72

 

Armament:

4x underwings pylons, each with a load capability of up to 2.000 lb (950 kg),

typically occupied with 400 US gal drop tanks or ALQ-76 Tactical Jamming System (TJS)

ECM pods. Other potential loads: AN/ALE-43(V)1&4 Bulk Chaff Dispensing System pod,

a single AN/AAQ-28(V) Litening targeting pod or AGM-45 Shrike anti-radar missiles

2x launch rails for defensive AIM-9 Sidewinder AAMs on the outer pylons

  

The kit and its assembly:

This what-if project had been lingering for a long time in the back of my mind, and I shoved it a side for years because of the model’s sheer size that eats up a lot of display space – even though I had the hardware already stashed away, collecting dust. While the build was rather inspired by its livery (see below) I wondered why the Vigilante, an elegant and impressive aircraft, had not been adapted to the ECM role? The concept of a supersonic penetrator/protector aircraft was realized by the USAF with the EF-111A Raven, but in the Vigilante’s time frame, the Vietnam War, esp. its end phase, an escort for fast USN attack aircraft might have made sense, so that I tried to mate the RA-5C with contemporary ECM technology and typical details – and the result became the fictional EA-5D.

 

With this idea the model became only a conversion of a basic airframe, not a spectacular kitbashing. Since I knew the Hasegawa RA-5C and its underwhelming quality/detail, I settled for the Trumpeter kit – a MUCH better but also a bit über-complicated offering. It is, however, better in any respect, even though you can ask why the cockpit has to consist of no less than thirty (!) parts (including seats and dashboard films), and the pylons as well as even the thin stabilizers and the fin have to consist of halves? One can also wonder why the kit comes with four(!) free-fall nukes but none of the RA-5C’s typical 400 gallon drop tanks? The kit features the type’s underwing flare dispensers, though. If there is something to criticize it’s the lack of air intake ducts – behind the wedge-shaped intakes and their ramps there is nothing inside the fuselage. Since I did not want to put too much effort into that flaw I simple blocked sight into the model’s body with a bulkhead made from black foamed styrene.

Everything goes together quite well, except for the fuselage halves which appear somewhat warped, and the rather massive plastic makes work easy. Despite this splendor of material, the sandwich leading and trailing edges are surprisingly thin and look pretty good.

 

While the RA-5C was at its core built OOB there were – naturally – some external mods to convey its ECM role. Most obvious detail is the fin top fairing, procured from a KiTech EA-6B, a shabby copy of the Hasegawa kit. This also provided the ECM pods and the pair of voluminous drop tanks.

The retrofitted Sidewinder launch rails on the outer pylons came from an Emhar FJ-4B, the then-state-of-the-art all-aspect AIM-9Ls came from a Hasegawa F-4 kit. To emphasize its electronic mission I added some antenna fairings around the hull. Beyond the fin pod, the EA-5D received sensor fairings along the flanks, inspired by the USAF F-105Gs’arrangement along the bomb bay, a shallow dorsal bulge behind the cockpits and some blister and blade antennae all around the hull.

 

The large ventral fairing that replaced the RA-5C’s “camera canoe” was scratched from a drop tank half, from a chunky Kangnam MiG-31, in an attempt to create something that the reminds of the EF-111’s arrangement. A ventral adapter for a display holder was integrated into the hull, too, for in-flight scenes.

A pair of long stabilizer fins was added under the rear fuselage, too, because I think that the large tail fin pod could somewhat hamper directional stability… The consist of rotor blades from a Matchbox SA.360 Dauphin helicopter.

The Vigilante’s tail cone, the former fairing for the linear bomb bay between the engines, was also heavily modified, with a thimble-shaped radome and a separate fairing for an internal chaff dispenser underneath, for a different look. To make the model look a bit more lively, esp. in its all-grey low-viz livery (see below) I mounted the flaps (all six are separate elements, and the inner pairs consist of lower and upper halves, too!) in lowered position.

  

Painting and markings:

The original reason to build this whiffy Vigilante was to see how the sleek and elegant aircraft would look in early USN low-viz colors! With this idea in mind the scheme was improvised and very simple: FS 36320 on the upper surfaces and FS 36375 underneath (Humbrol 128 and 127, respectively), on the flanks (with a relatively high waterline) and the fin. A slightly darker blue grey (FS 35237, Humbrol 145) was used for an anti-glare panel in front of the windshield. Most di-electric panels and the nose radome were painted in brownish light grey (RAL 7032, Revell 75), for low contrast but a significantly different color.

 

Inside, the landing gear as well as the air intakes were painted gloss white, the cockpit was painted in neutral grey (FS 36231) with dark grey ejection seats. The latter appears a bit tone-in-tone with the all-grey outside, but that was apparently the A-5’s interior design in real life.

 

To add some variety to the grey livery I painted the ordnance in “old” USN colors: the drop tanks became all-white and the ECM pods also received a white base. The AIM-9Ls on the extra launch rails (also painted white) received blue bodies as training missiles, with black seeker heads and white tail fins.

The wings’ leading edges (bare steel?) were masked and then painted with Revell 91 (iron metallic).

 

The whole model received a washing with thinned black ink to emphasize the many recessed rivets and panel lines, and then I added panel counter shading with lighter basic tones, also trying to create a slightly worn/weathered and not-so-uniform finish on the large grey surfaces, which underline the Vigilante’s elegant lines but also look quite boring, due to the sheer size/area, esp. from above.

 

The low-viz markings were improvised and puzzled together from various sources. The Red Stars on the fin were inspired by real-world aggressor markings, AFAIK some A-7Ls, EA-3Bs and A-4Fs carried such decorations, even paired with large bort numbers on the nose.

To improve the worn/grimy look I also treated the model’s surfaces with grinded graphite – only lightly, but I wanted to make the large grey areas to look even more diverse than just with the initial paint effects.

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

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).

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.

+++ 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!

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/

 

The computerized green markings send signals to her controller.

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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