Lockheed Martin X-35

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Lockheed Martin X-35 JSF
The X-35A JSF performs flight tests at Edwards Air Force Base, California
Type Prototype/Demonstrator
Manufacturer Lockheed Martin Aeronautics
Northrop Grumman
BAE Systems
Maiden flight 2000
Introduced NA
Status Retired (Museum)
Primary user Defense Advanced Research Projects Agency (DARPA)
Produced NA
Number built 2
Variants F-35 Lightning II
X-35C
Enlarge
X-35C

The X-35 was a experimental aircraft by Lockheed Martin for the Joint Strike Fighter Program. It was declared with winner over the Boeing X-32 and went on to enter production in the early 21st century as the F-35 Lightning II.

Contents

[edit] Development

The Joint Strike Fighter evolved out of several requirements for a common fighter to replace existing types. The actual JSF development contract was signed on November 16, 1996.

The contract for System Development and Demonstration (SDD) was awarded on 26 October 2001 to Lockheed Martin, whose X-35 beat the Boeing X-32. DoD officials and the UK Minister of Defence Procurement said the X-35 consistently outperformed the X-32, although both met or exceeded requirements.

The contract for System Development and Demonstration (SDD) was awarded on October 26, 2001 to Lockheed Martin, whose X-35 beat the Boeing X-32. DoD officials and the UK Minister of Defence Procurement said the X-35 consistently outperformed the X-32, although both met or exceeded requirements.

[edit] Specifications (X-35)

X-35A being refuelled in-flight by a KC-135 Stratotanker
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X-35A being refuelled in-flight by a KC-135 Stratotanker

General characteristics

  • Crew: pilot
  • 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 (42.7 m²)
  • Empty: 26,455 lb (12,000 kg)
  • Loaded: 41,900 lb (19,000 kg)
  • Maximum takeoff: 50,000 lb (22,680 kg)
  • Powerplant:

Performance

  • Maximum speed: km/h ( mph) Mach 1.8
  • Range: 620 miles (1000 km) without drop tanks
  • Service ceiling: 48,000 ft (15,000 m)
  • Rate of climb: m/min ( ft/min)
  • Wing loading: 91.4 lb/ft² (446 kg/m²)
  • Thrust/weight: 6.2 N/kg

[edit] Further reading

  • Spick, Mike (2002), The Illustrated Directory of Fighters. Salamander ISBN 1-84065-384-1

[edit] External links

[edit] Related content

Related development

Comparable aircraft

Designation sequence

Related lists

See also