F-35 Joint Strike Fighter Design Manfacturing Responsibilites

The primary customers are the United States armed forces and the United Kingdom ( RN and RAF), but the Netherlands, Australia, Turkey, Denmark, Norway, Singapore, Canada, ItalyThe Italian Republic or Italy ( Italian: Italia is a country in the south of Europe, consisting mainly of a boot-shaped peninsula together with two large islands in the Mediterranean Sea: Sicily and Sardinia. To the north, where it borders France, Switzer and IsraelThis article discusses the State of Israel. For other meanings of Israel see Israel (disambiguation). The State of Israel Medinat Yisrael in Hebrew, Daulat Israil in Arabic) is a country in the Middle East on the eastern edge of the Mediterranean Sea. are also participating in the program.

1 Design

The JSF planes are being constructed in three different variants to suit the needs of various users — a conventional take-off and landing aircraft (CTOL) for the U.S. Air ForceThe United States Air Force USAF is the aviation branch of the United States armed forces. The mission of the USAF is "to defend the United States through the control and exploitation of air and space. Organization There are three components of the USAF:; a carrierUSS John C. Stennis (left), and HMS Illustrious (right), showing the difference in size between a supercarrier and a typical aircraft carrier. An aircraft carrier is a warship whose main role is to deploy and recover aircraft. Aircraft carriers thus allow based variant (CV) for the U.S. NavyThe United States Navy USN is the branch of the United States armed forces responsible for naval operations. Navy consists of slightly fewer than 300 ships and over 4,000 operational aircraft. It has over a half million men and women on active or ready re; and a short take-off and vertical landing ( STOVLSTOVL is an acronym for S hort T ake O ff and V ertical L anding. This is the ability of some aircraft to take off from a short runway, and land vertically (i. with no runway). The most famous example is probably the Hawker Harrier Jump Jet, which though) aircraft for the U.S. Marine CorpsThe United States Marine Corps USMC is the second-smallest of the five branches of the United States armed forces, with 170,000 active and 40,000 reserve Marines as of 2002. The United States Coast Guard is the smallest. The Marine Corps is nonetheless la and the Royal Navy.

1.1 Manfacturing responsibilites

2 Program History

The Joint Advanced Strike Technology (JAST) program was created in 1993 as a result of a 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 a common family of aircraft to replace several aging U.S. and UK aircraft of which the JSF is one such example.

The JSF is a multi-role attack and fighter aircraft designed to replace the aging F-16 Fighting Falcon, F/A-18 Hornet, A-10 Thunderbolt II, F-111 Aardvark, Sea Harrier, Harrier GR7/GR9 and AV-8B Harrier jets. It will complement the USAF's high-end F/A-22 Raptor air superiority fighter and the U.S. Navy's F/A-18E/F Super Hornet as well as Europe's Eurofighter.

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. The construction contract 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, U.S. Department of Defense 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. While Boeing adopted the direct lift system, as in the Harrier, the X-35 generates vertical thrust through the use of the Rolls Royce LiftFan and a thrust-vectoring exhaust nozzle. The LiftFan alone generates 18,000 lb_f of thrust, compared to the 21,500 lb_f thrust of the Harrier's Pegasus engine. 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.

3 Analysis of JSF Program

Critics of the program maintain that the JSF suffers from ill-defined design goals; that it has insufficient internal fuel and weapon capacity to make a capable replacement for dedicated bombing aircraft; that its inability to supercruise limits it as an air defence platform, and that it is almost certain to suffer lengthy development delays and cost over-runs — 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. Several nations, however, 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 aircraft 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 aren't being allowed during the JSF development.

In 2004, it emerged that the JSF was indeed suffering development delays and cost blowouts, with the total projected cost of the program rising 23 percent to $244 billion. The major technical problem was the STOVL F-35B variant's mass, which was reported to be 8 percent over the target level (over 2200 pounds), which meant that the plane was projected as not being able to meet performance requirements. The Air Force CTOL F-35C variant and the Navy carrier-based variant were both within weight limits, but the F-35B was to be requested by the U.S. Marine Corps and the Royal Navy.

Lockheed Martin eventually solved the weight issues, shedding over a ton, and adding thrust. Several steps were taken to achieve this weight reduction, including reducing the thickness of the aircraft's skin, reducing the size of the weapons bay and vertical tails, redesigning the wing-mate joint, portions of the electrial system, and the portion of the aircraft immediately behind the cockpit, and lastly, rerouting some thrust from the roll-post outlets to the main nozzle. The smaller weapons bay will mean that the F-35B cannot carry Mark 84 2,000lb bombs, but this is typically not necessary in the envisioned close air support role.

USAF has elected to buy three wings (representing 216 examples) of the F-35B, as a result. This would seem to guarantee availability of the F-35B for the Marine Corps and the Royal Air Force. For a time, it appeared that the USAF variant of the F-35B would contain enough changes to constitute a new variant. 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 refuelling system. However, due to opposition from people involved with the program, the USAF version will be essentially identical to the USMC/Royal Navy F-35B specification.

Some of the international partners in the project have also become somewhat skittish, with Norway reportedly considering switching their purchase to the Eurofighter Typhoon or Saab Gripen because Norwegian industry had not been offered substantial enough involvement.

The Australian government and defence establishment has remained solidly behind the project. However, a number of concerns about the state of the project have been raised in various media outlets. Firstly, the delays in the schedule 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-18 fighters. The cost blowouts have also raised worries about the fleet's affordability. There has been considerable annoyance about the fact that the Australian planes will be less stealthy than the American versions, which, combined with concerns about the plane's short range, lack of supercruise and unproven dogfighting capabilities, have led to worries about its suitability to replace both the F-18 and F-111.

One important development has been the emergence of the USAF requirement for the F-35B. The STOVL variant had been viewed as the most likely victim of cost-cutting measures, however the USAF commitment seems to guarantee the aircraft that the USMC, Royal Navy, 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.

4 Variants

F-35A: conventional land-based version for USAF (potentially RAF)
F-35B: STOVL for USMC, RAF and RN (potentially USAF)
F-35C: carrier-based version for USN (potentially RN)

While all three versions had an initial slate of intended users, the situation is now somewhat fluid. With real-world performance of the Harrier being seen as positive, USAF is considering the F-35B. The Royal Navy is considering ordering the F-35C variant for its large CVF carriers.

Reportedly, versions for some countries other than the U.S. and U.K. may be subject to some export restrictions and be equipped with different mission systems. What equipment would be changed, and the difference in capabilities is not known.

5 Characteristics

Powerplant:
- Pratt & Whitney F135 turbofan rated at 156 kN maximum thrust; military thrust classified, possibly about 117 kN.
- General Electric/Rolls-Royce F136 Secondary powerplant
Size:
- Length: 15.47 m
- Height: 5.28 m
- Wingspan: 10.05 m
- Wing area: F-35A and F-35B: 42.7 m²; F-35C: 57.6 m²

Weight:
- Empty: 12,010 kg
- Normal Takeoff: 19,000 kg (?)
- Maximum: 22,680 kg
Speed:
- Maximum: Mach 1.7 at altitude,
Ceiling: about 15 km.
Range:
- Operational radius: 1000 km (I assume this is without drop tanks, as including them would make it less stealthy)
- Ferry: ? km
Wing Loading: F-35A: 446 kg/m² at 19,000 kg
Thrust/weight ratio: F-35A: 6.2 N/kg at 19,000 kg
Armament:
- one internal cannon (F-35A only, type undetermined; possibly M61A2 Vulcan)
- 4 AAMs with a mix of AIM-132 ASRAAM and AIM-120 AMRAAM

Cost: planned costs, in millions of 1994USD: F-35A: 28, F-35B: 35, F-35C: 38
First flight: 2000
In service date: expected to be 2008–2010
Users: USA (USAF, USN, USMC); UK (RAF, RN); others

6 See also

7 Further reading

Spick, Mike (2002), The Illustrated Directory of Fighters. Salamander BooksEnthsiast.com

8 External links

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Related Lists	List of military aircraft of the United States - List of fighter aircraft - List of experimental aircraft

US fighter aircraft 2000-2009 US attack aircraft 2000-2009 Carrier-based aircraft Stealth aircraft VTOL aircraft

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