Lockheed Martin X-35

Airplanes

Length

15.3924 m

Flat Wing Span

10.0584 m

Height

4.0538 m

Flat Wing Area

41.8064 m²

Max Mach

1.5 Mach

Max Ceiling

15240 m

Number of Engines

Aircraft Engine

First Flight

2000-10-24

Number Built

Maximum Take-Off Weight

22.6796 t (paragliders: kg)

Maximum Range

2222.4 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
Lockheed Martin X-35	22.6796	2222.4

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Mitsubishi F-2		15.52	11.125		Compare
Republic XF-84H Thunderscreech	Allison T40	15.67	10.18		Compare
Spartan C4		15.24	9.7536	2	Compare
Sukhoi Su-17 (1949)		15.253	9.6		Compare
General Dynamics F-16 Fighting Falcon	General Electric F110	14.9352	9.7536		Compare
General Dynamics X-62 VISTA	General Electric F110	14.8	9.8		Compare

All data (20 fields)

Name: Lockheed Martin X-35
Manufacturer: Lockheed Martin
Description: The Lockheed Martin X-35 is a concept demonstrator aircraft (CDA) developed by Lockheed Martin for the Joint Strike Fighter program.
First Flight: 2000-10-24
Designer: Lockheed Martin
Type: Concept demonstrator aircraft (CDA)
Length (m): 15.3924
Height (m): 4.0538
Cockpit Crew: 1
Max Ceiling (m): 15240
Max Mach (Mach): 1.5
Number Built: 2
Powerplant Description: 1 × Pratt & Whitney JSF119-PW-611 augmented turbofan
Primary Users: Defense Advanced Research Projects Agency (DARPA)
Status: Developed into the F-35
Wikipedia Article (URL): en.wikipedia.org/wiki/Lockheed_Martin_X-35
Flat Wing Span (m): 10.0584
Flat Wing Area (m²): 41.8064
Aircraft Engine: Pratt & Whitney F135
Number of Engines: 1