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Boeing
X32 JSF (2 pics)
Hovering test, photo: Boeing Boeing X-32 Mockup Leeuwarden AFB Netherlands July 2001, Rob Vogelaar
Hovering test, photo: Boeing
The Joint Strike fighter
(JSF) is a program designed to develop a family of stealthy, next- generation
replacement strike fighter aircraft for the USAF, USN, USMC and the UK Royal
navy and Royal Air Force.
The Joint Advanced Strike Technology program
ended its research phase in December 1994.
The JSF program entered its current phase, the Concept
Demonstration Phase in November 1996, when two contractors, Boeing (X-32)
and Lockheed Martin (X-35), were selected to build and fly Concept-
Demonstration aircraft.
There were two aircraft, the X-32A CTOL concept demonstrator for the USAF
and US Navy, and the X-32B STOVL concept demonstrator for the USMC and Royal
Navy. Unlike the Lockheed Martin X-35, there were no airframe changes required
to demonstrate US Navy aircraft carrier (CV/CTOL) approach capabilities - the
X-32A performed both roles.
First flight of the Boeing
X-32A was on September 18, 2000 a flight from Palmdale, CA to Edwards Air Force
Base, CA.
The first air-air refueling
with a McDonnell Douglas KC-10A Extender was on December 19, 2000.
With the X-32A were planned
for the test program, 30 flights conventional take-off and landing and 30
flights of carrier capable take-off and landings.
The X-32B first flight March
29,2001, completed the first vertical landings following transition from
conventional to vertical flight at the US Navy's Patuxent River, MD, test
facility at June 27, 2001. Since March 2001 it has flown 78 flights, 43,2 hours
in the test program, that ended on July 8,2001.
The Governments Joint Strike
Fighter decision on October 26, 2001, was a disappointment for Boeing, the
winner of the competition is the Lockheed Martin X-35. (F-35 Lightning II)
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Developing Nation: |
United
States of America. |
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Manufacturer/Designer: |
Boeing
Military Airplanes. |
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Task: |
Technology
demonstrator. |
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First Flight: |
- X-32A
September 18, 2000.
- X-32B
March 29,2001.
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Crew: |
1 |
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Wing
Span: |
- X-32A
10,97 m.
- X-32B
9,14 m. |
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Wing
Area: |
54,81 m². |
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Length: |
- X-32A
13,72 m.
- X-32B
13,33 m. |
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Height: |
4,06 m. |
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Engine (s): |
-
X-32A:
one Pratt & Whitney F-119-611
-
X-32B: one Rolls
Royce/Allison shaft-driven lift-fan
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Weight: |
-
Empty: X-32A/B 10.200 Kg.
X-32C 11.100 Kg.
- Internal
fuel: X-32A/B 6.800 Kg.
X-32C 7.700 Kg.
- External
weapons: 5.000 Kg.
X-32C 5.450 Kg. |
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Max.
Take off weight: |
-
X-32A/B 22.680 Kg.
- X-32C 27.200 Kg. |
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Max. ceiling: |
15.240 m. |
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Max. Speed: |
mach
1.5. |
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Max.
Range: |
-
X-32A 1.575 Km.
- X-32B 1.110 KM
- X-32C 1.390 Km. |
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g limits: |
9 + |
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Underwing
hardpoints: |
4. |
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Weapons: |
- 20mm M61A2 rotary
cannon.
- AIM-9 Sidewinder.
- AIM-120C AMRAAM.
-
Joint Direct Attack Munitions. |
Research: Rob Vogelaar
Last page update © zap16.com:
11-Oct-2007
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