Lockheed Martin F-35 Lightning II
The F-35 Joint Strike Fighter (JSF) is a military fighter aircraft designed by the USA and the United Kingdom. It is intended to replace the current generation of strike fighters, particularly the vertical take off and landing Harrier jump jets : the AV-8 Harrier II (US), Harrier GR7/9 (UK), and the Sea Harrier (UK), along with the conventional A-10 Thunderbolt II, F/A-18 Hornet and the F-16 Fighting Falcon. It is set to be a multi-role strike fighter (a plane with a strong emphasis on close air support and tactical bombing as well as being capable of air-to-air combat), currently in production with Lockheed Martin, along with partners Northrop Grumman and BAE Systems.
Three variants are envisioned: the conventional takeoff and landing (CTOL) F-35A for the U.S. Air Force (USAF) and the RAF; the Advanced Short Take-Off Vertical Landing (ASTOVL) F-35B for the U.S. Marine Corps (USMC) and the Royal Navy (RN); and the carrier-based (CV) F-35C for the U.S. Navy (USN). The USAF is considering the F-35B, and the Royal Navy is considering ordering the F-35C variant for its large CVF Future Carrier program.
The F-35, expected to be ready for service in 2008, is scheduled to begin replacing Marine Corps AV-8B Harrier and F/A-18s in 2009, and the USAF A-10 Thunderbolt II and F-16 in 2010.
International participation
The primary customers are the armed forces of the United States (USAF, USN, and USMC) and the United Kingdom (RAF and RN). There are three levels of international participation for the eight countries contributing to the program. The United Kingdom is the sole level I partner, contributing a little over $2 billion. Level II partners are Italy and the Netherlands, contributing $1 billion and $800 million respectively. At level III are Turkey ($175 million), Australia ($144 million), Norway ($122 million), Denmark ($110 million), and Canada ($100 million). The levels generally indicate the financial stake in the program, the level of technology transfer and subcontracts open for bid by national companies, and the general order in which countries can obtain production aircraft. Israel and Singapore have also joined as Security Cooperative Participants. [1]
The biggest international partner, the United Kingdom, has invested two billion in development funding for the project. Britain has also worked for five years for an ITAR waiver to allow greater technology transfer associated with the project. The effort, backed by the Bush administration, has been repeatedly blocked by U.S. Congressman Henry Hyde because of his concern about potential technology transfer to third countries. [2]
The CEO of BAE Systems, the British contractor on the plane, has complained that the U.S. has not given the UK (and his company) access to the crucial source code of the plane's software, thus making it impossible for the UK to maintain and modify the JSF independently. At a news conference at the Paris Air Show, he has even suggested that the UK may withdraw from the program unless additional access is granted, though analysts consider this unlikely [3]. On 21 December 2005 an article was published in the Glasgow Herald saying that MPs viewed as "unacceptable" the U.S. refusal to grant access to the source code. The article quotes the chairman of the Commons Defence Select Committee as saying that unless the UK receives assurances of access to the software information, "the UK might have to consider whether to continue in the programme".[4] Nonetheless, UK production commenced on 2 February 2006. [5]
International participants have at various times been cited as considering withdrawing from the JSF Program in favor of other aircraft such as Eurofighter Typhoon, Gripen or Rafale. Perceived inequitable sharing in JSF production is most often cited as the reason for considering withdrawal, rather than cost or performance concerns.
Program history
The Joint Advanced Strike Technology (JAST) program was created in 1993 as a result of a United States Department of Defense (DoD) Bottom-Up-Review. The major tactical aviation results of the review were to continue the ongoing F-22 and F/A-18E/F programs, cancel the Multi-Role Fighter (MRF) and the A/F-X programs, curtail F-16 and F/A-18C/D procurement, and initiate the JAST Program.
The JAST program office was established on January 27, 1994. It was established to define and develop aircraft, weapon, and sensor technology that would support the future development of tactical aircraft. The final goal was to replace several aging U.S. and UK aircraft with a common family of aircraft, of which the JSF is one example.
It will complement the USAF's high-end F-22 Raptor air superiority fighter and the USN's F/A-18E/F Super Hornet as well as Europe's Eurofighter.
Concept demonstration
The contract for development of the prototypes was awarded on 16 November 1996 to Lockheed Martin and Boeing, under which each was to produce two aircraft which were to demonstrate Conventional Take Off and Landing (CTOL), carrier take off and landing (CV version), and Short Take Off and Vertical Landing (STOVL).
Also in 1996 the UK Ministry of Defence launched the Future Carrier Borne Aircraft project, a replacement for the Sea Harrier (and later the Harrier GR7), for which the Joint Strike Fighter was selected in January 2001.
System development and demonstration
The construction contract, System Development and Demonstration (SDD), was awarded on 26 October, 2001 to the Lockheed Martin X-35, beating the Boeing X-32. The first planes are expected to enter service in 2008. Announcing the decision, DoD officials and the UK Minister of Defence Procurement said that while both aircraft met or exceeded requirements, the X-35 outperformed the Boeing aircraft consistently. This dominance can only have been achieved by Lockheed's method of STOVL flight; in fact, the decision is said to have clinched the contract.
Design
- Stealth technology
- Integrated avionics and sensor fusion - This allows information from off board sensors to be combined with those on-board the aircraft, to enhance the pilot's situational awareness and improve precision weapon delivery.
- Low construction cost
- Low maintenance cost
The rival Boeing X-32 adopted the relatively elegant Direct Lift System, where the exhaust gases were redirected to thrust vectoring nozzles to achieve lift during a STOVL landing. However, the X-35 utilized the far more complex Remote Shaft-Driven Fan concept, where extra LP turbine expansion developed additional power which was diverted, via a clutch-and-bevel gearbox, to a vertically mounted, contra-rotating, remote fan. The airstreams of both the remote fan and the normal fan were exhausted through thrust vectoring nozzles to provide lift during the STOVL landing phase. This method has the additional benefit of lowering environmental effects during (primarily) landing, where the thermal effects on, for example, a carrier deck are greatly reduced. In effect, the X-35 power plant acted as a flow multiplier and consequently had more than sufficient thrust for lift operations. The same cannot be said for the X-32 power plant, where even though the fan was oversized and throttle-pushed, it had insufficient thrust for lift. Because of the large engine airflow, the X-32 required a huge front air intake, compromising the aesthetics of the aircraft's aerodynamics. According to critics, Boeing designed an airplane "only its mother would love", in direct violation of the maxim "if it looks good, it flies good". Both the X-32 and X-35 power plants were derived from Pratt & Whitney F119, with the STOVL variant of the latter incorporating Rolls Royce Lift Fan module.
Note also that elements of the JSF design were pioneered by the F-22. The airframe appears quite similar to the F-22, albeit somewhat reduced in size, and only has a single engine.
Advanced weapons
The direct lift fan assembly, when not installed, provides approximately 100 ft3 of space [6], along with more than 27,000 hp (20 MW) available for electrical power production [7]. This has made directed-energy weapons possible for the F-35. Some of these designs, including solid state lasers and high-power microwave beams, are thought to be nearing operational status [8].
Possible reduction to two primary variants
Experts predicted in 2005 that the JSF program's Conventional Take-off and Landing [CTOL] F-35A variant may be canceled by acting U.S. Deputy Defense Secretary Gordon England. [9] This would not immediately save money in the program as the preproduction F-35A prototypes are already under construction, but long term, this cancellation could free up enough money to ensure that the program's F-35B and F-35C variants survive in the United States' tightening defense budget. Since then a flurry of lobbying from the JSF contractors, the Air Force, and representatives from the United Kingdom has convinced Secretary England and the DoD to stick with the 3-variant program.
Had such a cancellation occurred, the United States Air Force would stay in the program by purchasing either the STOVL F-35B for its close air support capabilities, the F-35C for its greater range, or a combination of the two. However, buys of these variants would likely be less than the 1000+ CTOL originally envisioned by the Air Force, as both variants cost more. This would have been a boon for A-10 and F-16 supporters, since those aircraft would probably be retained longer to compensate.
Export partners who were already wary of the JSF's rising costs showed some concern over a potential CTOL cancellation. Even the UK, which has no CTOL JSF requirement, lobbied to preserve that variant in order to keep costs of the others down. In the long run, the F-35B and F-35C should still be appealing to at least some of the international market, being the only fifth-generation program with a STOVL variant for countries in need of Harrier replacements.
Analysis of JSF program
Critics of the program maintain that the JSF suffers from ill-defined design goals; that it has insufficient range to make a capable replacement for dedicated bombing aircraft; that its inability to supercruise limits it as an air defense platform, and that it is almost certain to suffer lengthy development delays and cost overruns; meaning that interim types will have to be purchased to fill the gap between the end of useful life of existing fleets and the introduction of the JSF. However, it is important to note that the multi-role design philosophy has been tested and proven in combat over a period of at least 25 years, with successful types like the F-16 Fighting Falcon and the F-18 Hornet. Several nations, mainly current F-16 and F-18 users, already have sufficient confidence in the design to have committed substantial sums to become minority partners in the JSF manufacturing team.
The program's advocates see the JSF as an opportunity to break out of the decades-old pattern of U.S. military aircraft procurement: instead of a traditional per-service design approach, the JSF is being developed jointly by the Air Force, Navy and Marine Corps. This allows an estimated 80% commonality between the JSF variants for the different services, lowering procurement and service costs. This follows to a degree the philosophy behind the SEPECAT Jaguar and Panavia Tornado international development programs, the latter being called a multi-role combat aircraft (or MRCA) prior to service entry. Additionally, JSF is the first U.S. aircraft program to consider cost as independent variable (CAIV). In earlier programs the aircraft cost has been a dependent variable; additional features have always increased the aircraft cost. Such design changes are not being allowed during the JSF development.
Non-vehicle differentiator
A ground-based information system (the Autonomic Logistic Information System, or ALIS), built by Lockheed Martin Simulation Training and Support, is intended to make the JSF less expensive to operate and maintain.
Cost/weight issues
Through 2004 the JSF's total projected cost had risen 23% to $244 billion. The major technical problem was the F-35B variant's mass, which was reported to be 2,200 pounds, or 8%, over the target, which meant that the STOVL plane was projected to miss performance requirements.
Lockheed Martin eventually solved the weight problem by adding engine thrust and shedding over a ton by thinning the aircraft's skin; shrinking the F-35B weapons bay and vertical tails; redesigning the wing-mate joint, portions of the electrical system, and the portion of the aircraft immediately behind the cockpit; and rerouting some thrust from the roll-post outlets to the main nozzle. [10]
The smaller weapons bay will limit F-35B to 2 x 1000 lb (450 kg) weapons internally (this is as originally planned, for the 2 x 2000 lb requirement was added later). This is not expected to be a hindrance in close air support missions, which are likely to take place after enemy air defenses are down. Still, this may make the B variant different from the other two, boosting costs.
The internal weapons are stored offline to the external air flow, which will make for some interesting weapons certification work. The JSF has yet to drop a bomb, fire a missile, or fire a gun airborne—no demonstrations of weapons delivery capability were done during the "winner take all" fly off prior to contract award.
USAF STOVL purchase
The JSF program is not immune from interservice politics. A recurring theme has been the potential for a USAF requirement for the F-35B. The STOVL variant had been viewed as the most likely victim of cost-cutting measures; however, a USAF "commitment" seems to guarantee the aircraft that the USMC, RN, and RAF need. It is understood that the U.S. military's experience in Afghanistan has highlighted the importance of more flexible assets in the close air support role.
The USAF has investigated buying up to three wings (representing 216 examples) of the F-35B. For a time it appeared that the hypothetical USAF variant of the F-35B would contain enough changes to constitute a new variant (an F-35D). Changes were to include differences in the propulsion system to increase emphasis on STOL capability over that of VTOL, a larger wing to allow more fuel, an interior cannon (as opposed to the USMC external gun pod), or changes to the in-flight refueling system. However, due to opposition from people involved with the program, and the associated cost of developing a fourth variant, the USAF version would likely be identical to the USMC/RN F-35B specification.
Australian Participation
In May 2005 the Australian government announced that it was delaying a final decision on the JSF from the initial 2006 decision date to 2008 (and thus past the term of the present government). There are some concerns amongst Australian media, lobby groups and politicians, who have raised doubts that the aircraft will be ready in time to replace the aging Australian air force fleet of F-111 ground attack planes and F/A-18 fighters.
Concerns have been raised over cost efficiency, dog fighting capability, short range and lack of supercruise. The government also claims that the cost of purchasing mature F-22s may not be that much greater than the JSF. (Refer related discussions and analyzes on Air Power Australia web site.)
It should be noted on this claim that Jane’s Defence weekly recently (in 2005) put the value of an F-22 at $151 million dollars U.S., rising to $200 million if upgrades to approach the F-35's air to ground targeting performance were included. At a projected price of $45 million U.S. (2003 dollars), the F-35 is three to four times cheaper than the F-22. Therefore, there would have to be a very significant cost blowout in the F-35 program for the F-22 to become better value for money.
See also the article on Comparison of 21st century fighter aircraft.
Specifications (F-35 Joint Strike Fighter)
Some information is estimated.
General Characteristics
- Crew: 1
- Length: 50 ft 6 in (15.37 m)
- Wingspan: 35 ft 0 in (10.65 m)
- Height: 17 ft 4 in (5.28 m)
- Wing area: 459.6 ft² (42.7m²)
- Empty weight: 26,000 lb (12,000 kg)
- Loaded weight: 42,000 lb (19,000 kg)
- Maximum gross takeoff weight: 50,000 lb (23,000 kg)
- Powerplant: 1× Pratt & Whitney F135 afterburning turbofan, 37,100 lbf (165 kN)
- Secondary (High Performance), discontinued in current budget proposal[11]: 1x General Electric/Rolls-Royce F136 afterburning turbofan 178 kN thrust
- Lift fan (STOVL): 1x Rolls-Royce Lift System in conjunction with either F135 or F136 power plant 18,000 lbf (80 kN) thrust) each
Performance
- Maximum speed: Mach 1.8 (1,200 mph, 2,000 km/h)
- Cruise speed: Mach (mph, km/h)
- Range: 620 miles (1,000 km)
- Service ceiling: 48,000 ft (15,000 m)
- Climb rate: 40,000 ft/min[12] (2,000 m/s)
- Wing loading: 91.4 lb/ft² (446 kg/m²)
- Thrust/weight: 0.63:1
- Cost: (in millions US$):
- F-35A: 45
- F-35B: 60
Armament
- The F-35A will carry an internal GAU-12/U 25 mmm cannon, mounted under a blister on the port intake dorsal surface, with 180 rounds of ammunition. The F-35B and F-35C will carry the same weapon in a removable pod mounted on the aircraft's centerline, with 220 rounds of ammunition.
- To allow the aircraft to carry ordnance while maintaining low observability, the F-35 has two internal weapons bays, each capable of carrying one AIM-9X Sidewinder, AIM-120 AMRAAM or AIM-132 ASRAAM air-to-air missile, plus either one additional air-to-air missile or up to 2,000 lb (F-35A, F-35C) or 1,000 lb (F-35B) in air-to-ground stores, including but not limited to AGM-154 JSOW glide bombs (single weapon), Brimstone anti-armor missiles (triple packs), JDAM guided bombs (single weapon), GBU-39 Small Diameter Bomb quad packs, and the WCMD cluster bombs (single weapon). The MBDA Meteor air-to-air missile is currently being adapted to fit inside the weapons bays and my be integrated into the F-35.
- In addition, the F-35 can carry weapons externally on six under-wing hardpoints. On the two innermost hardpoints on each wing, the F-35 may carry "outsize" weapons that do not fit in the weapons bays, including but not limited to the Storm Shadow and AGM-158 JASSM cruise missiles and the AGM-88 HARM anti-radiation missile, in addition to the available stores for internal carriage. On the outermost hardpoints, the F-35 will carry short-ranged air-to-air missiles (Sidewinder or ASRAAM).
Other
- Cost: (in millions US$):
- F-35A: 45
- F-35B: 60
- Costing as per Asia Pacific Defence Reporter, September 2005.
- F-35C: 55
- First flight - X-35 demonstrator: 2000
- Expected first flight F-35A - September 2006
- In-service date: expected to be 2009 through 2012. The reason for this is that the A will be brought into service first followed by the B. The C will be in service in 2012.
Manufacturing responsibilities
- Lockheed Martin Aeronautics (prime contractor)
- Final assembly
- Overall system integration
- Mission system
- Forward fuselage
- Wings
- Northrop Grumman
- Active Electronically Scanned Array (AESA) radar
- Center fuselage
- Weapons bay
- Arrestor gear
- BAE Systems
- Aft fuselage and empennages
- Horizontal and vertical tails
- Crew life support and escape
- Electronic warfare systems
- Fuel system
- Flight Control Software (FCS1)
Media
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Further reading
- Spick, Mike (2002), The Illustrated Directory of Fighters. Salamander ISBN 1-84065-384-1
- Kopp, Carlo; Goon, Peter, Australian Aviation, JSF related articles.
Notes and References
- ^ Katherine V. Schnasi Joint Strike Fighter Aquisition: Observations on the Supplier Base US Accounts Office. Retrieved Feb. 08, 2006.
- ^ Spiegel, Peter, MSNBC UK denied waiver on US arms technology. Financial Times (MSNBC reprint). Retrieved Feb. 08, 2006.
- ^ Fletcher,Matthew; Katz,Alan (June 16, 2005). U.K. May Miss Out on Technology From U.S. Fighter. Bloomberg.com. Retrieved Feb. 08 , 2006.
- ^ UK Defense Committee Statement MoD 'slippage' set to leave forces with reduced capability, says committee UK Parliament. Retrieved Feb. 08, 2006.
- ^ Helen Jocelyn Lift-Off as production starts on first STOVL F-35 BAE Systems. Retrieved Feb.08, 2006.
- ^ Morris, Jefferson (Sept. 26, 2002). Keeping Cool A Big Challenge For JSF Laser, Lockheed Martin Says. Aerospace Daily Retrieved Feb. 08, 2006.
- ^ Fulghum, David A. (July 8, 2002). Lasers Being Developed for F-35 and AC-130. Aviation Week and Space Technology Retrieved Feb. 08, 2006.
- ^ Fulghum, David A. (July 22, 2002). Lasers, HPM Weapons Near Operational Status. Aviation Week and Space Technology Retrieved Feb. 08, 2006.
- ^ Selinger, Marc (Nov. 21, 2005). [U.S. Air Force's JSF Variant May Be Killed, Expert Says. Aviation Week and Space Technology Retrieved Feb. 08, 2006.
- ^ Fulghum, David A.; Wall, Robert (Sept.19, 2004). USAF Plans for Fighters Change. Aviation Week and Space Technology Retrieved Feb. 08, 2006.
- ^ The exact statistic is classified.
- ^ Watson, Ian (22 Jan. 2006). Bush rejects Blair’s pleas to save F-35 contract for Rolls-Royce. Business Online, UK Retrieved Feb. 08, 2006.
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