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EADS MAKO
The EADS Mako/High Energy Advanced Trainer (Mako/HEAT) was a high-performance jet trainer or light attack aircraft intended for service with several European air forces. EADS proposed the Mako for the Eurotrainer program. The program was the final result of the AT-2000 project. Design and development The Mako design featured a single aft-mounted jet engine, fed by two air intake ramps at the roots of the mid-fuselage-wing. It features a trapezoidal wing with a sharp taper. The horizontal tail was an all-flying unit mounted close behind the wing and at nearly the same height. The retractable landing gear was a tricycle unit. The two occupants shared a highly streamlined bubble canopy. Subcontractors would have included Diehl Aerospace, Aermacchi (now Leonardo), Saab, EAB and Dassault Aviation. The Mako shows remarkable stealth aircraft features, partially due to faceting and partially due to composite materials, using some results from the MBB Lampyridae stealth p ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
EADS
Airbus SE (; ; ; ) is a European multinational aerospace corporation. Airbus designs, manufactures and sells civil and military aerospace products worldwide and manufactures aircraft throughout the world. The company has three divisions: '' Commercial Aircraft (Airbus S.A.S.)'', '' Defence and Space'', and ''Helicopters'', the third being the largest in its industry in terms of revenues and turbine helicopter deliveries. As of 2019, Airbus is the world's largest airliner manufacturer. The company's main civil aeroplane business is conducted through the French company Airbus S.A.S., based in Blagnac, a suburb of Toulouse, with production and manufacturing facilities mostly in the European Union and the United Kingdom but also in China, the United States and Canada. Final assembly production is based in Toulouse, France; Hamburg, Germany; Seville, Spain; Tianjin, China; Mobile, United States; and Montreal, Canada. The company produces and markets the first commercially viable ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
General Electric F414
The General Electric F414 is an American afterburning turbofan engine in the 22,000- pound (98 kN) thrust class produced by GE Aviation. The F414 originated from GE's widely used F404 turbofan, enlarged and improved for use in the Boeing F/A-18E/F Super Hornet. The engine was developed from the F412 non-afterburning turbofan planned for the A-12 Avenger II, before it was canceled. Design and development Origins GE evolved the F404 into the F412-GE-400 non-afterburning turbofan for the McDonnell Douglas A-12 Avenger II. After the cancellation of the A-12, the research was directed toward an engine for the F/A-18E/F Super Hornet. GE successfully pitched the F414 as a low-risk derivative of the F404, rather than a riskier new engine. The F414 engine was originally envisioned as not using any materials or processes not used in the F404, and was designed to fit in the same footprint as the F404."Confident GE heads to F414 CDR next month" (1994). ''Aerospace Daily''. Vol 169, No. 34; ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
IRIS-T
The IRIS-T ("thermography, InfraRed Imaging System Tail/thrust vectoring, Thrust Vector-Controlled") is a medium range infrared homing missile available in both air-to-air missile, air-to-air and ground defence surface-to-air missile, surface-to-air variants. The missile was developed in the late 1990s–early 2000s by a German-led program to develop a short to medium range infrared homing air-to-air missile to replace the AIM-9 Sidewinder in use by some NATO member countries at the time. A goal of the program was for any aircraft capable of firing the Sidewinder to also be capable of launching the IRIS-T. The air-to-air variant was fielded in 2005. Surface-to-air missile, Surface-to-air missile defense, defence systems variants came later, with the short-range IRIS-T SLS fielded in 2015, and the medium-range IRIS-T SLM fielded in 2022. One IRIS-T SLM battery, as supplied by Germany to Ukraine, consists of three truck-mounted launchers, carrying eight missiles each (with a ran ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
AIM-9 Sidewinder
The AIM-9 Sidewinder (where "AIM" stands for "Air Intercept Missile") is a short-range air-to-air missile which entered service with the US Navy in 1956 and subsequently was adopted by the US Air Force in 1964. Since then the Sidewinder has proved to be an enduring international success, and its latest variants remain standard equipment in most Western-aligned air forces. The Soviet K-13 (AA-2 'Atoll'), a reverse-engineered copy of the AIM-9B, was also widely adopted by a number of nations. Low-level development started in the late 1940s, emerging in the early 1950s as a guidance system for the modular Zuni rocket. This modularity allowed for the introduction of newer seekers and rocket motors, including the AIM-9C variant, which used semi-active radar homing and served as the basis of the AGM-122 Sidearm anti-radar missile. Originally a tail-chasing system, early models saw extensive use during the Vietnam War but had a low success rate. This led to all-aspect capabilities in ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
GBU-24
GBU-24 Paveway III or simply GBU-24 is a family of laser-guided bombs, a sub-group of the larger Raytheon Paveway III family of weapons. The Paveway guidance package consists of a seeker package attached to the nose of the weapon, and a wing kit attached to the rear to provide stability and greater range. Warhead options consist of: * Mk. 84 – General Purpose * BLU-109 – Penetrator * BLU-116 – Advanced Unitary Penetrator * CPE-800 – Used in the BPG-2000, a similar, indigenous Spanish weapon Compared to the GBU-10 family, or the Paveway II family, the GBU-24 glides farther as a result of more efficient guidance technology. The Paveway III guidance kit is more expensive, however, making the GBU-24 suitable against well-defended, high-value targets. It was introduced into service c. 1983. This weapon is in service with the USAF, US Navy, US Marine Corps, and various NATO air forces. The bomb requires a spot of pulse-coded laser energy to home on; this can be ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
GBU-16
The GBU-16 Paveway II is an American Paveway-series laser-guided bomb, based on the Mk 83 general-purpose bomb, but with laser seeker and wings for guidance. The GBU-16 was introduced into service around 1976 and is used by the U.S. Air Force, U.S. Navy, U.S. Marine Corps, and various NATO air forces. GBU-16 bombs are produced by Lockheed Martin and Raytheon. Raytheon began production after purchasing the product line from Texas Instruments. Lockheed Martin was awarded a contract to compete with Raytheon when there was a break in production caused by transferring manufacturing out of Texas. Raytheon production of the GBU-16 is centered in Arizona, Texas, and New Mexico. Lockheed Martin's production is centered in Pennsylvania. Laser Guided Bombs are often labeled as "smart bombs" despite requiring external input in the form of laser designation of the intended target. According to Raytheon's fact sheet for the PAVEWAY 2, 99 deliveries of guided munitions will yield a circu ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Mk 83
The Mark 83 is part of the Mark 80 series of low-drag general-purpose bombs in United States service. Development and deployment The nominal weight of the bomb is 1,000 lb (454 kg), although its actual weight varies between 985 lb (447 kg) and 1,030 lb (468 kg), depending on fuze options, and fin configuration. The Mk 83 is a streamlined steel casing containing 445 lb (202 kg) of tritonal high explosive. When filled with PBXN-109 thermally insensitive explosive, the bomb is designated BLU-110. The Mk 83/BLU-110 is used as the warhead for a variety of precision-guided weapons, including the GBU-16 Paveway laser-guided bombs, the GBU-32 JDAM and Quickstrike sea mines. The Mk 83 is also used as the warhead in a variety of Pakistani smart bombs made by GIDS. During Operation Swift Retort in 2019, 2 JF-17 Thunders of the No. 16 Squadron "Black Panthers" armed with newly developed Mk. 83 Range Extension Kit (REK) bombs struck military target ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Mk 82
The Mark 82 (Mk 82) is an unguided, low-drag general-purpose bomb, part of the United States Mark 80 series. The explosive filling is usually tritonal, though other compositions have sometimes been used. Development and deployment With a nominal weight of , it is one of the smallest in current service, and one of the most common air-dropped weapons in the world. Although the Mk 82's nominal weight is 500 lb, its actual weight varies depending on its configuration, from . It is a streamlined steel casing containing of Tritonal high explosive. The Mk 82 is offered with a variety of fin kits, fuzes, and retarders for different purposes. The Mk 82 is the warhead for the GBU-12 laser-guided bombs and for the GBU-38 JDAM. Currently only the General Dynamics plant in Garland, Texas and Nitro-Chem in Bydgoszcz, Poland are Department of Defense-certified to manufacture bombs for the US Armed Forces. The Mk 82 is currently undergoing a minor re ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Turbofan
The turbofan or fanjet is a type of airbreathing jet engine that is widely used in aircraft engine, aircraft propulsion. The word "turbofan" is a portmanteau of "turbine" and "fan": the ''turbo'' portion refers to a gas turbine engine which achieves mechanical energy from combustion, and the ''fan'', a ducted fan that uses the mechanical energy from the gas turbine to force air rearwards. Thus, whereas all the air taken in by a turbojet passes through the combustion chamber and turbines, in a turbofan some of that air bypasses these components. A turbofan thus can be thought of as a turbojet being used to drive a ducted fan, with both of these contributing to the thrust. The ratio of the mass-flow of air bypassing the engine core to the mass-flow of air passing through the core is referred to as the bypass ratio. The engine produces thrust through a combination of these two portions working together; engines that use more Propelling nozzle, jet thrust relative to fan thrust are ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
