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Lockheed Martin F-35 'Lightning II' (2 pics)
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 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.
The JSF program entered
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.
The first
flight of the X-35A was at 24 October 2000 with LMTAS test pilot Tom Morgenfeld.
The X-35A test-program ended November 22, 2000 after 27 test-flights and is
rebuild as the X-35B.
The X-35B
Short-take-off/vertical-landing (STOVL) variant, with its unique shaft-driven
lift-fan propulsion system, achieved its first vertical take-off and vertical
landing on June 23, 2001.
The
X-35C first flight February 12, 2001 is the carrier variant, completed 250
practice carrier landings at Naval Air Station Patuxent River, MD.
This is the Navy version of the JSF will be similar to the Air Force version
except with a stronger internal structure, landing gear, bigger wing, and
arresting hook to allow carrier landings.
The US Department of
Defense announced on October 26, 2001, Lockheed Martin as the winner of the JSF
program.
During System Development and Demonstration
(SDD) phase of the JSF program, the 22 JSF test aircraft (14 of which will have
full-flight capability) will undergo an extensive series of ground and flight
tests for the Pentagon to establish their compliance with contract
specifications. The official production order is expected to be issued to
Lockheed Martin in 2006. Both SDD contract performance and partner-country order
quantities are factors contributing to future teammate production-order
decisions. Approximately 4,500 aircraft are expected to be built.
The first CTOL F-35A has begun airframe
assembly at July 12, 2004 and the first wing assembly at August 23, 2004, and is
scheduled for its first flight in August 2006. The STOVL F-35B first flight is
set for 2007. The F-35A fighter is expected to enter service in 2008, the F-35B
in 2012.
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.
Video of all F-35 Versions, including the Vertical take off.
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Developing Nation: |
United
States of America. |
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Manufacturer/Designer: |
Lockheed
Martin. |
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Task: |
Radar-evading, supersonic
multi-role fighter. |
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First
Flight: |
- X-35A October 24, 2000.
- X-35B June 23, 2001.
- X-35C February 12, 2001. |
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Lockheed Martin X-35
Joint Strike Fighter |
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Crew: |
1 |
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Wing
Span: |
- X-35A 10,00 m.
- X-35C 13,12 m (9,90 m folded). |
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Length: |
- X-35A 15,41 m.
- X-35C 15,50 m. |
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Height: |
4,07 m. |
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Engine
(s): |
-
X-35A/C: one Pratt & Whitney F-119-611 turbo-fan.
-
X-35B: one Rolls-Royce/Allison shaft-driven lift-fan.
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Weight: |
-
Empty: 9.980 Kg.
- Max. load: 22.680 Kg. |
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Max.
Take off weight: |
9.980 Kg. |
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Max. Speed: |
mach
1.5. |
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Max.
Range: |
3.000 km. |
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g limits: |
9 + |
X-35A:

X-35B:

X-35C:

Images Lockheed
Martin.
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Lockheed Martin F-35
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First
Flight: |
- F-35A 2006.
- F-35B 2007.
- F-35C 2006. |
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First
Delivery: |
- F-35A 2008.
- F-35B 2012.
- F-35C 2010. |
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Initial
operational capability dates: |
- US Marine
Corps: autumn 2010
- US Air Force: autumn 2011
- US Navy: autumn 2012
- Royal Navy/Royal Air Force: 2012 |
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Crew: |
1 |
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Ejection Seat: |
Martin
Baker. |
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Wing
Span: |
- F-35A 10,65 m.
- F-35B 10,65 m.
- F-35C 13,11 m. |
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Wing
Area: |
- F-35A 42,7 m².
- F-35B 42,7 m².
- F-35C 57,6 m². |
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Length: |
- F-35A 15,37 m.
- F-35B 15,37 m.
- F-35C 15,48 m. |
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Height: |
4,57 m. |
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Engine: |
- One Pratt and Whitney
afterburning turbofan F-135 engine with 164,6kN thrust.
- the F-35B engine is
coupled with a shaft-driven lift fan system for STOVL propulsion. |
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Weight: |
-
Empty: Kg.
- Internal fuel: F-35A
8.300 Kg.
F-35B 6.080 Kg.
F-35C 8.663 Kg.
- Max. payload: 6.805 Kg. |
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Max.
Take off weight: |
27.215 Kg. |
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Max. Speed: |
Mach 1.6+ |
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Max.
Range: |
- F-35A 1.300 Km.
- F-35B 920 Km.
- F-35C 1.480 Km. |
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g limits: |
9+. |
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Radar: |
AN/APG-81
multi-function radar. |
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Centerline
hardpoint('s): |
1. |
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Underwing
hardpoints: |
3 each wing. |
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Wingtip
hardpoints |
1 each
wingtip. |
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Weapons
of the
F-35 in two internal weapon bays: |
- Mausers 27 mm cannon.*
- AIM-9X Sidewinder.
- AIM-120 AMRAAM.
-
Joint Direct Attack Munitions
- CBU-105 WCMD
(Wind- Corrected Munitions Dispenser) for the Sensor-Fuzed Weapon.
- JSOW (Joint Stand
Off Weapon).
- Paveway II guided
bombs.
- 455 kg
bombs and 900 kg bombs. |
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External weapons provided for non- stealthy missions: |
-
AIM-9X Sidewinder.
- JASSM (Joint Air-to-Surface Standoff
Missile).
- Storm Shadow cruise missile. |
* The
F-35's Air Force version would have its gun mounted internally, while the Navy
and Marine Core
versions' could be set underneath the aircraft.
Lockheed Martin wins $200 Billion
contract from Pentagon, the biggest in history, Pratt & Whitney $4, 8 Billion
contracts for the engine. The production should be in Fort Worth, Texas.
Estimated
cost:
F-35A $40
million
F-35B $50
million
F-35C $50
million
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Development Partners |
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USA |
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United Kingdom |
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Level 2 |
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Italy |
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Netherlands |
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Level 3 |
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Turkey |
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Canada |
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Norway |
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Denmark |
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Australia |
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Security Co-operation
Participant |
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Israel |
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Singapore |
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Production planning: |
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USAF. |
- 1763 |
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USMC. |
- 609 |
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USN. |
- 480 |
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RAF/Navy. |
- 150 |
Lockheed Martin immediately
started the 126 month-long SDD phase (System Development and Demonstration),
which involves the construction of 14 flight test aircraft and 8 test articles:
- 5 x CTOL aircraft
- 4 x STOVL aircraft, two for flight sciences and two for mission system
testing
- 5 x CV aircraft
- 6 x static test articles for fatigue and load tests
- 1 x CTOL pole test model for cross section measurement
- 1 x CV drop test airframe
LRIP 1
production (10 aircraft) should start in mid-2006, followed by LRIP 2 (22
aircraft) in 2007, LRIP 3 (54 aircraft) in 2008, LRIP 4 (91 aircraft) in 2009,
LRIP 5 (120 aircraft) in 2010 and LRIP 6 (168 aircraft) in 2011.
Research: Rob Vogelaar
Last page-update © zap16.com
30-Dec-2008
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