Thursday, April 10, 2008

United Kingdom Ministry of Defence - AgustaWestland EH101


The AgustaWestland EH101 (AW101 from June 2007) is a medium-lift helicopter for military applications but also marketed for civil use. The helicopter was developed as a joint venture between Westland Aircraft in the UK and Agusta in Italy (now merged as AgustaWestland). The name Merlin is used for EH101s in British and Portuguese military service.

The designation "EH101" is a typographical error that stuck: the aircraft was originally designated EHI (European Helicopter Industries) - 01. The aircraft is manufactured at the AgustaWestland factories in Yeovil, England and Vergiate in Italy.

The modular aluminium-lithium alloy fuselage structure is damage and crash resistant, with multiple primary and secondary load paths. Active vibration control of the structural response (ACSR) uses a vibration-cancelling technique to reduce the stress on the airframe. The EH101 is rated to operate in temperatures ranging from -40 to +50 °C. High flotation tyres permit operation from soft or rough terrain. The main rotor blades are a derivative of the BERP blade design, which improves the aerodynamic efficiency at the blade tips, as well as reducing the blade's noise signature.

The cockpit is fitted with armoured seats for the crew, and can withstand an impact velocity of over 10 m/s. Dual flight controls are provided, though the EH-101 can be flown by a single person. The pilot's instrument displays include six full colour high-definition screens and an optional mission display. A digital map and Forward-Looking Infrared system display can also be installed.

In spring 1977, the UK Ministry of Defence issued a requirement for an anti-submarine warfare (ASW) helicopter to replace the Royal Navy's Westland Sea Kings. Westland responded with a design designated the WG.34 that was then approved for development. Meanwhile, the Marina Militare (Italian Navy) was also seeking a replacement for its (Agusta-built) Sea Kings, leading Agusta to discussions with Westland about the possibility of a joint development. This culminated in the joint venture being finalised in November 1979 and a new company (EH Industries Limited [EHI], based in London) being formed in June the following year to manage the project.

As the design studies progressed, EHI became aware of a broader market for an aircraft with the same capabilities as those required by the British and Italian navies. On 12 June 1981, the UK confirmed their participation, with an initial budget of £20 billion to develop nine pre-series examples. At the 1985 Paris Air Show at Le Bourget, Agusta showed a mock-up of a utility version of the new helicopter, leading to a more generalised design that could be customised. After a lengthy development, the first prototype flew on October 9, 1987.

EHI was renamed AgustaWestland International Limited in January 2004 when parent companies merged. Consequently, in June 2007, the EH101 was re-branded as the AW101.

United Kingdom Ministry of Defence - BAE Hawk

The BAE Systems Hawk is a British advanced jet trainer which first flew in 1974 as the Hawker Siddeley Hawk. It is used by the Royal Air Force, and other air forces, as either a trainer or a low-cost combat aircraft. The Hawk is still in production with over 900 Hawks sold to 18 customers around the world.

n 1964 the Royal Air Force specified a requirement for a new initial jet trainer to replace the Folland Gnat. The SEPECAT Jaguar was originally intended for this role, but it was soon realised that it would be too complex an aircraft for initial jet training. Accordingly, in 1968 Hawker Siddeley began the design of a much simpler strictly subsonic trainer, the HS.1182. It was to have tandem seating and would be capable of carrying armaments, which would enable it to be used as a weapons trainer and in light combat roles.

Renamed "Hawk" in 1973, the aircraft first flew in 1974. It entered RAF service in April 1976, replacing the Gnat and Hawker Hunter in the advanced training and weapons training roles respectively. The following year Hawker Siddeley merged with other British aircraft companies to form the nationalised British Aerospace (BAe), which subsequently became BAE Systems upon merger with Marconi Electronic Systems in 1999.

The most famous RAF operator of the Hawk is the Red Arrows aerobatic team, which adopted the plane in 1979. The Finnish Air Force aerobatics team, the Midnight Hawks, also uses the aircraft.

The Hawk has excellent maneuverability, and while it is not capable of supersonic speed in level flight, it can attain Mach 1.2 in a dive, allowing trainees to experience trans-sonic handling without the cost of a supersonic trainer.

The Hawk subsequently replaced the English Electric Canberra in the target towing role.

The Royal Navy acquired a dozen Hawk T.Mk 1/1As from the RAF, for use as aerial targets for the training of ships gunners and radar operators.

United Kingdom Ministry of Defence - Westland WAH-64 Apache


The WAH-64 is a licence-built version of the Boeing AH-64D Apache Longbow attack helicopter, for the British Army. The first eight helicopters were built by Boeing, the remaining 59 were assembled by Westland at Yeovil from kits purchased from Boeing. The WAH-64 is designated Apache AH Mk 1 or AH1 by the UK's Ministry of Defence.

The UK's Strategic Defence Review called for Apaches to undertake amphibious attack missions, operating from the helicopter carrier HMS Ocean, the Invincible class aircraft carriers and their successors, the (Royal Navy CVF programme), and possibly the amphibious assault vessels HMS Bulwark and Albion. As such, one of the major differences between the WAH-64 and AH-64 Apache variants is the folding blade mechanism, required to stow the helicopters in the confined space onboard ships.

The Apache will serve aboard Royal Navy ships having achieved maritime certification in December 2005 aboard HMS Ocean. Then on November 17, 2006, HMS Ark Royal became the first RN aircraft carrier to land a WAH-64D Apache AH1 at Portsmouth Naval Base.

United Kingdom Ministry of Defence - Raytheon Sentinel


The Raytheon Sentinel is under development as the RAF's ASTOR (Airborne STand-Off Radar) aircraft. It will be a joint asset with the British Army, providing battlefield and ground surveillance in a similar role to the American E-8 JSTARS aircraft. ASTOR will be totally interoperable with allied systems such as JSTARS and the NATO Alliance Ground Surveillance (AGS) system.

The first flight of a modified Bombardier Global Express was in August 2001 which validated the modifications required for the ASTOR system. The first production Sentinel R1 made its 4.4 hour maiden flight on May 26 2004. The initial operating capability will be achieved in 2008.

The original contracts call for a total of five aircraft, eight mobile ground stations (six on wheeled all terrain vehicles and two in air transportable containers), and extensive training facilities at the main RAF station.

The ASTOR cockpit features a new centrally housed, pull-down screen capable of displaying a moving map, Link 16 datalink information and defensive aids subsystem (DASS) data.The DASS comprises a towed radar decoy, missile approach warning system and chaff and flare dispensers and can be operated in automatic, semi-automatic or manual mode.

The aircraft will normally fly at over 15,000 m (40,000 ft) to ensure a high resolution view of a large battlefield area. It will be crewed by a pilot, a co-pilot, an Airborne Mission Commander (AMC) and 2 image analysts. Mission endurance should be about 9 hours. While the image analysts can analyse the images on board the aircraft it is expected that, unlike the JSTARS, the actual battle management will occur on the ground.

The radar which provides this capability is supplied by Raytheon Systems Ltd. (RSL), the UK subsidiary of Raytheon. It is a next-generation dual-mode Synthetic Aperture / Moving Target Indication (SAR/MTI) radar based on proven technology previously used in Raytheon’s ASARS-2 system. The radar is installed on a heavily modified Bombardier business jet - the Global Express, which will be known as the Sentinel R1 in RAF service. The aircraft is powered by the same engines used in the Nimrod MRA4 upgrade programme, the Rolls-Royce BR710. The aircraft is based at RAF Waddington and operated by 5 Sqn.

The image to the right shows prototype 9001, a Global Express development aircraft belonging to Bombardier, carrying the external fairings and antennas of the radar and communications systems that will be fitted on the production aircraft. However it is substantially different in other areas, such as the number of portholes and military colours.

While suffering from delays the project is one of few procurement projects to be below cost estimates.

United Kingdom Ministry of Defence - Hawker Siddeley Nimrod


The Nimrod is a maritime patrol aircraft developed in the United Kingdom. It is an extensive modification of the de Havilland Comet, the world's first jet airliner. It was originally designed by de Havilland's successor, Hawker Siddeley, now part of BAE Systems. A major modification was the fit of a large weapon bay under the fuselage that can carry and drop torpedoes, mines, bombs and other stores. Sonobuoys for tracking submarines are dropped from special launchers in the rear of the fuselage.

It has been the Royal Air Force's primary Maritime Patrol Aircraft (MPA) since the early 1970s, when it replaced the piston-engined Avro Shackleton. The RAF uses two Nimrod variants: the MR2 variant in the Maritime and Reconnaissance role; the R1 variant in a reconnaissance and electronic intelligence gathering capacity (ELINT).

The Nimrod was the first jet-powered MPA of any significance. Earlier MPA designs used piston or turboprop engines to improve fuel economy and allow for lengthy patrols. Jet engines are most economical at high altitudes and less economical at low altitudes. However, the transit to the operational area can be made at high altitude and in a jet aircraft this is not only economical on fuel but fast as well, compared to earlier piston-powered aircraft. After transit, the Nimrod descends to its patrol area..

United States Department of Defense - F/A-18E/F Super Hornet


The Boeing F/A-18E/F Super Hornet is a supersonic carrier-based fighter/attack aircraft. The F/A-18E/F Super Hornet is a larger and more advanced derivative of the F/A-18C/D Hornet. The Super Hornet entered service with the United States Navy in 1999 and will serve alongside the original Hornet. It has been ordered by the Royal Australian Air Force in 2007 to replace its aging F-111 fleet.

The design of the Super Hornet may have gone through a more extensive evolution than any other combat aircraft. The F-5 Freedom Fighter donated its basic wing platform, enlarged wing root extensions, and nose as the starting point for the Northrop YF-17 Cobra lightweight fighter. The YF-17 was then sized up to produce the middle-weight F/A-18 multi-role fighter, which roughly matched the Phantom in range/payload and missile armament. The Super Hornet is about 20% larger, 7000 lb (3000 kg) heavier empty, and 15,000 lb (6800 kg) heavier at maximum weight than the original Hornet. Although the original YF-17 was about the same weight as the small F-5, the Super Hornet carries 33% more internal fuel, increasing mission range by 41% and endurance by 50% over the "Legacy" Hornet. The empty weight of the Super Hornet is about 11,000 lb (5000 kg) less than that of the F-14 Tomcat that it replaced.

United States Department of Defense - Boeing X-32


The Boeing X-32 was a multi-purpose jet fighter in the Joint Strike Fighter contest. It lost to the Lockheed Martin X-35 demonstrator which was further developed into the F-35 Lightning II.

In 1993, the Defense Advanced Research Projects Agency (DARPA) launched the Common Affordable Lightweight Fighter project (CALF). The project's purpose was to develop a stealth-enabled design to replace all of US DoD lighter weight fighter and attack aircraft, including the F-16 Fighting Falcon, F/A-18 Hornet, and STOVL short takeoff / vertical landing AV-8B Harrier II. Around the same time the Joint Advanced Strike Technology (JAST) project was started. In 1994, the US Congress ordered the two to be merged into the Joint Strike Fighter Program.

Many companies took part in the first phase of this project, which involved drafting concept aircraft designs for submission to the Department of Defense. However on 16 November 1996, only Boeing and Lockheed Martin were awarded contracts, allowing them to produce two of their concept aircraft each. Under the contract, these fighters were required to demonstrate Conventional Take Off and Landing (CTOL), carrier take off and landing (CV version), and Short Take Off and Vertical Landing (STOVL). They were also expected to include ground demonstrations of a production representative aircraft's systems, such as the Preferred Weapon System Concept (PWSC).

One major departure from previous projects was the prohibition of the companies from using their own money to finance development. Each was awarded $750 million to produce their two aircraft – including avionics, software and hardware. This limitation promoted the adoption of low cost manufacturing and assembly techniques, and also prevented either Boeing or Lockheed Martin from bankrupting themselves in an effort to win such an important contest.

United States Department of Defense - F-35 Lightning II


The Lockheed Martin F-35 Lightning II is a single-seat, single-engine, stealth-capable military strike fighter, a multi-role aircraft that can perform close air support, tactical bombing, and air-to-air combat. The F-35 is descended from the X-35 of the Joint Strike Fighter (JSF) program. Its development is being principally funded by the United States with the United Kingdom and other partner governments providing additional funding. It is being designed and built by an aerospace industry team led by Lockheed Martin with Northrop Grumman and BAE Systems as major partners.Demonstrator aircraft flew in 2000, with the production model first flying on 15 December 2006.

While the United States is the primary customer and financial backer, the United Kingdom, Italy, the Netherlands, Canada, Norway, Denmark, Australia and Turkey have contributed US$4.375 billion toward the development costs of the program. Total development costs are estimated at more than US$40 billion (underwritten largely by the United States), while the purchase of an estimated 2,400 planes is expected to cost an additional US$200 billion. The nine major partner nations plan to acquire over 3,100 F-35s through 2035, making the F-35 one of the most numerous jet fighters.

There are three levels of international participation. The levels generally reflect the financial stake in the program, the amount of technology transfer and subcontracts open for bid by national companies, and the order in which countries can obtain production aircraft. The United Kingdom is the sole "Level 1" partner, contributing US$2.5 billion, about 10% of the development costs under the 1995 Memorandum of Understanding that brought the UK into the project. Level 2 partners are Italy, which is contributing US$1 billion; and the Netherlands, US$800 million. Level 3 partners are Canada, US$440 million; Turkey, US$175 million; Australia, US$144 million; Norway, US$122 million; and Denmark, US$110 million. Israel and Singapore have joined as Security Cooperative Participants (SCP).

Some of the partner countries have wavered in their public commitment to the JSF program, hinting or warning that unless they receive more subcontracts or technology transfer, they will forsake JSF for the Eurofighter Typhoon, Saab Gripen, Dassault Rafale or simply upgrade their existing aircraft. Norway has several times threatened to put their support on hold unless substantial guarantees for an increased industrial share is provided. Despite this Norway has signed all the Memoranda of Understanding, including the latest one detailing the future production phase of the JSF program. They have, however, indicated that they will increase and strengthen their cooperation with both competitors of the JSF, the Typhoon and the Gripen.

Wednesday, April 9, 2008

United Kingdom Ministry of Defence - Eurofighter Typhoon


The Eurofighter Typhoon is a twin-engine multi-role canard-delta wing strike fighter aircraft. It is being designed and built by a consortium of three separate partner companies - Alenia Aeronautica, BAE Systems and EADS - working through a holding company Eurofighter GmbH which was formed in 1986. The project is managed by NETMA (the NATO Eurofighter and Tornado Management Agency) which acts as the prime customer. As early as 1979, studies began into what would become the Eurofighter Typhoon.

The series production of the Eurofighter Typhoon is now underway. The aircraft has entered service with the British Royal Air Force, the German Luftwaffe (Jagdgeschwader 74), Italian Air Force, and Spanish Air Force. Austria has purchased 15 Typhoons and Saudi Arabia has signed a GB£4.43 billion (approx. €6.4 billion c. 2007) contract for 72 aircraft.

United Kingdom Ministry of Defence - Queen Elizabeth class aircraft carrier


The Queen Elizabeth class aircraft carriers (formerly CVF) are a two-ship class of aircraft carrier being developed for the Royal Navy. The HMS Queen Elizabeth is expected to enter service in 2014, HMS Prince of Wales in 2016. The vessels will displace about 75,000 tonnes (full load).

The need to replace the ageing Invincible class aircraft carriers was confirmed by the 1998 Strategic Defence Review. From six contractors, the Ministry of Defence (MoD) selected Thales and BAE Systems in late 1999 to compete for the final contract. In September 2002 the MoD announced that the Royal Navy and RAF will operate the STOVL F-35B Lightning II variant and further that the carriers would take the form of large, conventional carriers, which will initially be adapted for STOVL operations. On January 30, 2003 the MoD announced that the Thales design had won the competition but that BAE Systems would operate as prime contractor. The two companies are now part of a "carrier alliance" with the MoD and other companies.

The contract for the vessels was announced on 25 July 2007 by the Secretary of State for Defence Des Browne, ending several years of delay over cost issues and British naval shipbuilding restructuring. The cost is estimated to be £3.9 billion.

United Kingdom Ministry of Defence - Albion class landing platform dock


The Albion class is a class of landing platform dock, and are the newest amphibious assault vessels in the Royal Navy fleet. The class consists of two vessels, HMS Albion and HMS Bulwark and they were ordered in 1996 under a programme known as LPD(R) (Landing Platform Dock (Replacement)) to replace the aging Fearless class. Both ships were built by BAE Systems Marine at the former VSEL yard in Barrow-in-Furness. Albion commissioned on June 19, 2003 and Bulwark on July 12, 2004.

The class gives the Royal Navy the ability to land heavy forces as the ships operate the Landing Craft Utility Mark 10, capable of taking a Challenger 2 tank or all other heavy armoured vehicles that the United Kingdom operates. The well deck can operate four such LCUs. The ships carry 305 military personnel on board in normal conditions and another 650 for short emergency periods. The vehicle decks are capable of carrying up to six Challenger 2 tanks, six L118 105 mm Light Guns and up to sixty-seven various support vehicles and trailers. They do not have hangars but have a 64-metre flight deck and landing spots capable of accepting a Chinook helicopter or two aircraft up to the size of the Merlin HC3 or Sea King HC4. Each ship operates a Hippo BARV (Beach Armoured Recovery Vehicle) to assist in landing operations. The Hippo is a conversion by ALVIS Moelv of a Leopard 1A5 tank into a military crawler tractor. The Hippo has a tractive effort of 250 kN (56,000 lbf), a fording depth of 2.95 m (9.7 ft) and can pull vehicles up to 50 tonnes weight or push off from the beach a 240 tonne displacement landing craft.

The class offers numerous improvements over their Fearless class predecessors and 60% of their equipment was new to naval service when introduced . The state-of-the-art Combined Operations Room which is an electronically advanced "amphibious battle-staff co-ordination cell" that has 72 workstations for the naval task group and amphibious landing forces. The class also features - the Royal Navy's first - integrated full electric propulsion system, reducing engine-room personnel by around two-thirds, allowing for a total reduction in personnel of 40%. The new Mark 10 LCU allows for roll-on/roll-off operations, assisting vehicle loading operations in the well deck.

United Kingdom Ministry of Defence - Astute class submarine


The Astute class submarines are the next generation nuclear fleet submarines of the Royal Navy. When completed, the boats will set a new standard for the Royal Navy in terms of weapons load, improved communications facilities, stealth and comfort for the crew. Lord Drayson (Former Minister for Defence Equipment and Support) said, "These submarines are hugely impressive vessels, and will provide the Royal Navy with a world class capability." The boats are being constructed by BAE Systems Submarine Solutions at Barrow-in-Furness.

As the Swiftsure-class submarines aged, the Royal Navy began to design their replacements. The original design called for large submarines designed for blue-water operations. Feasibility studies began in 1986 and were completed by 1989. A design contract was placed with Vickers Shipbuilding and Engineering Ltd. (VSEL) in 1987, but with the end of the Cold War the project was cancelled in 1992. Emphasis switched to the production of a second batch of Trafalgar-class submarines (Batch 2 Trafalgar Class or B2TC). However the development was extremely slow and initial tenders received from VSEL in June 1995 were too expensive.

Meanwhile, the Royal Navy has changed its submarine-employment strategy from the Cold War emphasis on anti-submarine warfare to the concept of "Maritime Contributions to Joint Operations." The proposed replacement boats were redesigned; the primary mission of the Astute class became direct support of surface forces.

Original plans were for seven boats of the Astute class to replace five Swiftsure-class submarines (Sovereign, Superb, Sceptre, Spartan, and Splendid) and the two oldest Trafalgar-class boats (Trafalgar and Turbulent). The Swiftsure-class will be entirely decommissioned by 2010, when only the first of the Astute-class will be coming into service. HMS Trafalgar is to be decommissioned in 2008, followed by HMS Turbulent in 2011.

Sunday, April 6, 2008

United Kingdom Ministry of Defence - Type 45 destroyer


The United Kingdom's Type 45 destroyer (also known as the D or Daring class) is a state of the art air defence destroyer programme of the Royal Navy. The first ship in the class, HMS Daring, was launched on February 1, 2006 and is expected to come into service in 2009. The ships are assembled by BAE Systems Surface Fleet Solutions from partially prefabricated "blocks" built by BAE and VT Group.

The UK originally sought to procure air defence ships as part of the 8 nation NFR-90 project and later the Horizon Common New Generation Frigate programme with France and Italy. The Type 45s take advantage of some Horizon development work and utilise the SAMPSON radar variant of the Principal Anti-Air Missile System - PAAMS(S).

After Daring's launch on 1 February 2006, former First Sea Lord, Admiral Sir Alan West stated that it would be the Royal Navy's most capable destroyer ever, as well as the world's best air defence ship. The Daring class represents the largest escort type ever built for the Royal Navy.

The Type 45 destroyers will be 152.4 m in length, with a beam of 21.2 m and a draught of 5.0 m. This makes them significantly larger than the Type 42 they replace, displacing about 7350 tonnes compared to 5200 tonnes of the Type 42. The Type 45 destroyers are the first British warships built to meet the hull requirements of Lloyd's Register's Naval Rules. BAE Systems is the Design Authority for the Type 45 a role traditionally held by the UK Ministry of Defence.

The Type 23 frigates were the first British warships to incorporate signature reduction technology, with the large 70° angle of the bow, the elimination of right angles and reduced equipment on deck. The propulsion system was also chosen to minimise noise, with electric generators providing minimal acoustic signature for anti-submarine warfare (ASW) missions and the infrared signature is reduced by cooling devices on the funnels. The design of the Type 45 builds upon the design of the Type 23. It brings new levels of signature reduction to the Royal Navy, with the reduced deck equipment producing a very "clean" superstructure similar to the La Fayette class of frigates. Life rafts and docking equipment are concealed behind superstructure panels and the mast is very sparingly equipped.

United Kingdom Ministry of Defence - Defence Equipment & Support

Defence Equipment and Support (DE&S) is the name of the merged procurement and support organisation within the UK Ministry of Defence
The new organisation has a civilian and military workforce of around 29,000 (77 per cent civilian and 23 per cent military), in the UK and abroad. DE&S operates as a single Top Level Budget.

United Kingdom Ministry of Defence


The Ministry of Defence (MoD) is the United Kingdom government department responsible for implementation of government defence policy and is the headquarters of the British Armed Forces.

The MoD states that its principal objective is to defend the United Kingdom and its interests. With the collapse of the Soviet Union and the end of the Cold War the MoD does not foresee any short-term conventional military threat; rather, it has identified weapons of mass destruction, international terrorism, and failed and failing states as the overriding threats to the UK's interests. The MoD also manages day to day running of the armed forces, contingency planning and defence procurement.

During the 1920s and 1930s, British civil servants and politicians, looking back at the performance of the state during World War I, concluded that there was a need for greater co-ordination between the three Services that made up the armed forces of the United Kingdom—the British Army, the Royal Navy, and the Royal Air Force. The formation of a united ministry of defence was rejected by Prime Minister David Lloyd George's coalition government in 1921; but the Chiefs of Staff Committee was formed in 1923, for the purposes of inter-Service co-ordination. As rearmament became a concern during the 1930s, Stanley Baldwin created the position of Minister for Coordination of Defence. Lord Chatfield held the post until the fall of Neville Chamberlain's government, in 1940; but his success was limited by his lack of control over the existing Service departments and his limited political influence.

Winston Churchill, on forming his government in 1940, created the office of Minister of Defence to exercise ministerial control over the Chiefs of Staff Committee and to co-ordinate defence matters. The post was held by the Prime Minister of the day until Clement Attlee's government introduced the Ministry of Defence Act of 1946. The new ministry was headed by a Minister of Defence who possessed a seat in the Cabinet. The three existing service Ministers — the Secretary of State for War, the First Lord of the Admiralty, and the Secretary of State for Air — remained in direct operational control of their respective services, but ceased to attend Cabinet.

From 1946 to 1964 five Departments of State did the work of the modern Ministry of Defence: the Admiralty, the War Office, the Air Ministry, the Ministry of Aviation, and an earlier form of the Ministry of Defence. These departments merged in 1964; the defence functions of the Ministry of Aviation Supply merged into the Ministry of Defence in 1971.

Wednesday, April 2, 2008

United States Department of Defense - V-22 Osprey


The V-22 Osprey is an American joint service, multimission, military tiltrotor aircraft with both a vertical takeoff and landing (VTOL) and short takeoff and landing (STOL) capability. It is designed to perform missions like a conventional helicopter with the long-range, high-speed cruise performance of a turboprop aircraft. The V-22 was developed by Bell Helicopter Textron, which manufactures it in partnership with Boeing Helicopters. The initial operators are the United States Marine Corps and Air Force. The FAA classifies the Osprey as a model of powered lift aircraft.
The Osprey is the world's first production tiltrotor aircraft, with one three-bladed proprotor, turboprop engine, and transmission nacelle mounted on each wingtip. For takeoff and landing, it typically operates as a helicopter with the nacelles vertical (rotors horizontal). Once airborne, the nacelles rotate forward 90° in as little as 12 seconds for horizontal flight, converting the V-22 to a more fuel-efficient, higher-speed turboprop airplane. STOL rolling-takeoff and landing capability is achieved by having the nacelles tilted forward up to 45°. For compact storage and transport, the V-22's wing rotates to align, front-to-back, with the fuselage. The proprotors can also fold in a sequence taking 90 seconds.
The V-22 is equipped with a glass cockpit, which incorporates four Multi-Function Displays (MFDs) and one shared Central Display Unit (CDU), allowing the pilots to display a variety of images including: digimaps centered or decentered on current position, FLIR imagery, primary flight instruments, navigation (TACAN, VOR, ILS, GPS, INS), and system status. The flight director panel of the Cockpit Management System (CMS) allows for fully-coupled (aka: autopilot) functions which will take the aircraft from forward flight into a 50-foot hover with no pilot interaction other than programming the system.
The V-22 is a fly-by-wire aircraft with triple redundant flight control systems. With the nacelles pointing straight up in conversion mode at 90° the flight computers command the aircraft to fly like a helicopter, with cyclic forces being applied to a conventional swashplate at the rotor hub. With the nacelles in airplane mode (0°) the flaperons, rudder, and elevator fly the aircraft like an airplane. This is a gradual transition which occurs over the entire 96° range of the nacelles. The lower the nacelles, the greater effect of the airplane-mode control surfaces.
The Osprey is armed with one 0.30 in (7.62 mm) machine gun pointing rearward that can be fired when the loading ramp is lowered. A GAU-19 three-barrel 0.50 in (12.7 mm) gatling gun mounted below the V-22's nose has also been studied for future upgrade. BAE Systems is also developing a remotely operated turreted weapons system for the V-22.

United States Department of Defense - UH-1N Twin Huey


The Bell UH-1N Twin Huey is a medium military helicopter that first flew in April, 1969. The UH-1N has a fifteen seat configuration, with one pilot and fourteen passengers. In cargo configuration the UH-1N has an internal capacity of 220 ft³ (6.23 m³). An external load of 5,000 lb (2,268 kg) can be carried by the UH-1N.
Based on the stretched fuselage Bell 205, the Bell 212 was originally developed for the Canadian Forces (CF) under the designation CUH-1N Twin Huey. Later the CF adopted a new designation system and the aircraft was re-designated as the CH-135 Twin Huey. The CF approved the development of the aircraft on May 1, 1968 and purchased 50 aircraft, with deliveries commencing in May 1971.
The US military came very close to not procuring the Twin Huey. The purchase of the aircraft for US military use was opposed by the Chairman of the House Armed Services Committee at the time, Mendal Rivers. Rivers took this position because the aircraft powerplant, the Pratt & Whitney Canada PT6T was produced in Canada. The Canadian government had not supported US involvement in Vietnam and had opposed US policies in southeast Asia, as well as accepting US draft dodgers. Rivers was also concerned that procurement of the engines would result in a negative trade deficit situation with Canada. Congress only approved the purchase when it was assured that a US source would be found for the PT6T engines. As a result the United States military services ordered 294 Bell 212s under the designation UH-1N, with deliveries commencing in 1970.
Unlike in the Canadian Forces, in US service, the UH-1N retained the official name "Iroquois" from the single engined UH-1 variants, although US service personnel refer to the aircraft as a "Huey" or "Twin Huey".

The Bell 412 is a further development of the Bell 212, the major difference being the composite four-blade main rotor.

Design


The UH-1N's main rotor is powered by a PT6T-3 Turbo Twin Pac made up of two Pratt & Whitney Canada PT6T turboshaft engines. They are capable of producing up to 1,342 kW (1,800 shp). Should one engine fail the remaining engine can deliver 671 kW (900 shp) for 30 minutes or 571 kW (765 shp) enabling the UH-1N to maintain cruise performance at maximum weight.

The United States Marine Corps (USMC) modified a large number of their UH-1Ns with a Stability Control Augmentation System (SCAS) which provides servo inputs to the rotor head to help stabilize the aircraft during flight. This modification removed the gyroscopic "Stabilization Bar" on top of the main rotor head, instead relying on the computer system for stability.