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Characteristics Summary (Jan. 25, 1950)

Lockheed XF-90 diagram.

Lockheed XF-90 diagram.

Characteristics Summary
25 January 1950

Fighter - XF-90:
Wing area = 350 sq. ft.
Span = 40.0 ft.
Length = 56.2 ft.
Height = 15.8 ft.

Status: 
1. Teletype Authorization: 11 April 1946
2. Contract Date: 20 June 1946
3. Mock-up Inspection: December 1947
4. Engineering Inspection: April 1949
5. First Flight: (1st Art.) 3 June 1946; (2nd Art.) March 1950 

Power Plant:
(2) XJ34-WE-11 Westinghouse 

ENGINE RATINGS

S.L. Static LB - RPM
Max: *4100 - 12500
Mil: 2920 - 12500
Nor: 2420 - 11800 

*with afterburners operating ATO

No & Model
(4) 12AS1000D4
Mfr Aerojet
Thrust Lb (ea) 1000
Duration (sec) 12

Features:
Crew: 1
Pressurization
Cooling & Heating
AN/APG-5 Radar
A-1B Gun-Bomb-Rocket Sight
Ejection Seat
Dive Brakes
Automatic Slats
Adjustable Stabilizer
Aileron Boost
Two-Position Fowler Flaps
Max fuel capacity: 1665 gal. 

Armament:
Turrets: None
Guns: 6 x 20mm
Ammunition (tot): 1602 rds.
Max Bomb Load: 2 x 1000 lb.
Max Bomb Size 1000 lb.
Rockets: 8 x 5" HVAR

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