Characteristics Summary (Jan. 25, 1950) Characteristics Summary25 January 1950Fighter - 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) 12Features: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