F-35 Lightning II - Joint Strike Fighter (JSF), International

F-35 Lightning II - Joint Strike Fighter (JSF), International (NSI News Source Info) December 3, 2008: The F-35 Lightning II joint strike fighter (JSF), is being developed by Lockheed Martin Aeronautics Company for the US Air Force, Navy and Marine Corps and the UK Royal Navy.

The first flight of the CTOL F-35A took place on 15 December 2006. JSF is being built in CTOL, carrier-based and STOVL variants. The stealthy, supersonic multi-role fighter was designated the F-35 Lightning II in July 2006. The JSF is being built in three variants: a conventional take-off and landing aircraft (CTOL) for the US Air Force; a carrier variant (CV) for the US Navy; and a short take-off and vertical landing (STOVL) aircraft for the US Marine Corps and the Royal Navy. A 70%-90% commonality is required for all variants. The requirement is for: USAF F-35A air-to-ground strike aircraft, replacing F-16 and A-10, complementing F-22 (1763); USMC F-35B – STOVL strike fighter to replace F/A-18B/C and AV-8B (480); UK RN F-35C – STOVL strike fighter to replace Sea Harriers (60); US Navy F-35C – first-day-of-war strike fighter to replace F/A-18B/C and A-6, complementing the F/A-18E/F (480 aircraft). In January 2001, the UK MoD signed a memorandum of understanding to co-operate in the SDD (system development and demonstration) phase of JSF and, in September 2002, selected the STOVL variant to fulfil the future joint combat aircraft (FJCA) requirement. Following the contract award, other nations signed up to the SDD phase are: Australia, Canada, Denmark, Italy, Netherlands, Norway, Singapore and Turkey. Concept demonstration phase The concept demonstration phase of the programme began in November 1996 with the award of contracts to two consortia, led by Boeing Aerospace and Lockheed Martin. The contracts involved the building of demonstrator aircraft for three different configurations of JSF, with one of the two consortia to be selected for the development and manufacture of all three variants. In October 2001, an international team led by Lockheed Martin was awarded the contract to build JSF. An initial 22 aircraft (14 flying test aircraft and eight ground-test aircraft) will be built in the programme's system development and demonstration (SDD) phase. Flight testing will be carried out at Edwards Air Force Base, California, and Naval Air Station, Patuxent River, Maryland. Aerial refuelling of the F-35A and concept demonstration phase of the programme began in November 1996. In April 2003, JSF completed a successful preliminary design review (PDR). The critical design review (CDR) for the F-35A was completed in February 2006, for the F-35B in October 2006 and for the F-35C in June 2007. The first flight of the CTOL F-35A took place on 15 December 2006. Low-rate initial production (LRIP) for the F-35A/B was approved in April 2007 with an order for two CTOL aircraft. An LRIP 2 contract for six CTOL aircraft was placed in July 2007. The STOVL F-35B was rolled out in December 2007 and made its first flight, a conventional take-off and landing, in June 2008. STOVL flights are to begin in early 2009. An LRIP contract for six F-35B STOVL aircraft was placed in July 2008. The F-35C is scheduled for first flight in mid-2009. The F-35A fighter is expected to enter service in 2010, the F-35B in 2012. The first flight of the F-35 powered by the GE Rolls-Royce F136 engine is scheduled for 2010 with first production engine deliveries in 2012. Critical design review was completed in February 2008. By the end of 2006, Australia, Canada, the Netherlands and the UK had signed the MoU for the F-35 Production, Sustainment and Follow-on Development (PSFD) phase. Norway and Turkey (requirement 100 F-35A) signed in January 2007. Denmark and Italy (requirement 131 F-35A and B) signed in February 2007. In May 2008, Israel requested the sale of 25 F-35A aircraft with 50 options. In September 2004, Lockheed Martin announced that, following concerns over the weight of the STOVL F-35B, design changes had reduced the aircraft weight by 1,225kg while increasing propulsion efficiency and reducing drag. The weight requirements will also call for a smaller internal weapons bay than on the other variants. The Lockheed Martin JSF team includes Northrop Grumman, BAE Systems, Pratt and Whitney and Rolls-Royce. Final assembly of the aircraft will take place at Lockheed Martin's Fort Worth plant in Texas. Major subassemblies will be produced by Northrop Grumman Integrated Systems at El Segundo, California and BAE Systems at Samlesbury, Lancashire, England. BAE Systems is responsible for the design and integration of the aft fuselage, horizontal and vertical tails and the wing-fold mechanism for the CV variant, using experience from the Harrier STOVL programme. Terma of Denmark and Turkish Aerospace Industries of Turkey are supplying sub-assemblies for the centre fuselage. Design In order to minimise the structural weight and complexity of assembly, the wingbox section integrates the wing and fuselage section into one piece. To minimise radar signature, sweep angles are identical for the leading and trailing edges of the wing and tail (planform alignment). The fuselage and canopy have sloping sides. The seam of the canopy and the weapon bay doors are sawtoothed and the vertical tails are canted at an angle. The marine variant of JSF is very similar to the air force variant, but with a slightly shorter range because some of the space used for fuel is used for the lift fan of the STOVL propulsion system. The F-35B counter-rotating lift fan, developed by Rolls-Royce, can generate more than 20,000lb of thrust. To minimise radar signature, sweep angles are identical for the leading and trailing edges of the wing and tail. The main differences between the naval variant and the other versions of JSF are associated with the carrier operations. The internal structure of the naval version is very strong to withstand the high loading of catapult-assisted launches and tailhook arrested landings. The aircraft has larger wing and tail control surfaces for low-speed approaches for carrier landing. Larger leading edge flaps and foldable wingtip sections provide a larger wing area, which provides an increased range and payload capacity. The canopy (supplied by GKN Aerospace), radar and most of the avionics are common to the three variants. Cockpit and avionics systems L-3 Display Systems is developing the panoramic cockpit display system, which will include two 10in x 8in active matrix liquid crystal displays and display management computer. The following will also supply F-35 avionics systems: *BAE Systems Avionics - side stick and throttle controls *Vision Systems International (a partnership between Kaiser Electronics and Elbit of Israel) - advanced helmet-mounted display *BAE Systems Platform Solutions - alternative design helmet-mounted display, based on the binocular helmet being developed for the Eurofighter Typhoon *Ball Aerospace - communications, navigation and integration (CNI) integrated body antenna suite (one S-band, two UHF, two radar altimeter, three L-band antennas in each aircraft) *Harris Corporation - advanced avionics systems, infrastructure, image processing, digital map software, fibre optics, high-speed communications links and part of the communications, navigation and information (CNI) system *Honeywell - radar altimeter, inertial navigation / global positioning system (INS/GPS) and air data transducers *Raytheon - 24-channel GPS with digital anti-jam receiver (DAR). Weapons Weapons are carried in two parallel bays located in front of the landing gear. Each weapons bay is fitted with two hardpoints for carrying a range of bombs and missiles. "Weapons are carried in two bays located in front of the landing gear." Weapons to be cleared for internal carriage include: JDAM (joint direct attack munition), CBU-105 WCMD (wind-corrected munitions dispenser) for the sensor-fused weapon, JSOW (joint stand-off weapon), Paveway IV guided bombs, small diameter bomb (SDB), AIM-120C AMRAAM air-to-air missile and Brimstone anti-armour missile; for external carriage: JASSM (joint air-to-surface stand-off missile), AIM-9X Sidewinder, AIM-132 ASRAAM and Storm Shadow cruise missile. In September 2002, General Dynamics Armament and Technical Products was selected as the gun system integrator. The air force variant has an internally mounted gun. The carrier and marine variants can have an external gun pod fitted. Targeting Lockheed Martin Missile & Fire Control and Northrop Grumman Electronic Sensors and Systems are jointly responsible for the JSF electro-optical system. A Lockheed Martin electro-optical targeting system (EOTS) will provide long-range detection and precision targeting, along with the Northrop Grumman DAS (distributed aperture system) thermal imaging system. EOTS will be based on the Sniper XL pod developed for the F-16, which incorporates a mid-wave third-generation FLIR, dual mode laser, CCD TV, laser tracker and laser marker. BAE Systems Avionics in Edinburgh, Scotland will provide the laser systems. DAS consists of multiple infrared cameras (supplied by Indigo Systems of Goleta, California) providing 360° coverage using advanced signal conditioning algorithms. As well as situational awareness, DAS provides navigation, missile warning and infrared search and track (IRST). EOTS is embedded under the aircraft's nose, and DAS sensors are fitted at multiple locations on the aircraft. Radar Northrop Grumman Electronic Systems is developing the advanced electronically scanned array (AESA) AN/APG-81 multi-function radar. The AN/APG-81AESA will combine an integrated radio frequency subsystem with a multifunction array. "A Lockheed Martin electro-optical targeting system (EOTS) will provide long-range detection and precision targeting." The radar system will also incorporate the agile beam steering capabilities developed for the APG-77. Northrop Grumman delivered the first radar to Lockheed Martin in March 2005 for flight testing. Countermeasures BAE Systems Information & electronic warfare systems (IEWS) will be responsible for the JSF integrated electronic warfare suite, which will be installed internally and have some subsystems from Northrop Grumman. BAE is developing a new digital radar warning receiver for the F-35. Systems Other suppliers will include: *ATK Composites - upper wing skins *Vought Aircraft Industries - lower wing skins *Smiths Aerospace - electronic control systems, electrical power system (with Hamilton Sundstrand), integrated canopy frame *Honeywell - landing system wheels and brakes, onboard oxygen-generating system (OBOGS), engine components, power and thermal management system driven by integrated auxiliary power unit (APU) *Parker Aerospace - fuel system, hydraulics for lift fan, engine controls and accessories *Moog Inc - primary flight control electrohydrostatic actuation system (EHAS), leading edge flap drive system and wing-fold system *EDO Corporation - pneumatic weapon delivery system *Goodrich - lift-fan anti-icing system *Stork Aerospace - electrical wiring Propulsion Early production lots of all three variants will be powered by the Pratt and Whitney afterburning turbofan F-135 engine, a derivative of the F119 fitted on the F-22. Following production aircraft will be powered by either the F135 or the F-136 turbofan being developed by General Electric and Rolls-Royce. However, in the 2007 US Military Budget, published in February 2006, no funding was allocated for the development of the F-136 engine. The US Congress voted to restore funding for the F-136 in October 2006. "DAS sensors are fitted at multiple locations on the joint strike fighter." Each engine will be fitted with two BAE Systems full authority digital electronic control (FADEC) systems. Hamilton Sundstrand is providing the gearbox. On the F-35B, the engine is coupled with a shaft-driven lift fan system for STOVL propulsion. The counter-rotating lift fan, developed by Rolls-Royce Defence, can generate more than 20,000lb of thrust. Doors installed above and below the vertical fan open as the fin spins up to provide vertical lift. The main engine has a three-bearing swivelling exhaust nozzle. The nozzle, which is supplemented by two roll control ducts on the inboard section of the wing, together with the vertical lift fan provide the required STOVL capability. Key Data F-35A (CTOL).................................Conventional take-off and landing for US Air Force F-35B (STOVL)Short take-off and landing for US Marine Corps, and the UK Navy and Air Force F-35C (CV).......................................Carrier variant for US Navy CTOL and STOVL............................15.4m Length CTOL and STOVL.............................4.6m Height CTOL and STOVL..............................10.6m Wingspan CV Length ............................................15.5m