In support of an official event 

The Museum will be closed Sunday, May 25
In addition, the Fourth Hangar will be closed Saturday, May 24

Access to the Presidential Gallery will be limited from May 15 to June 5
 

Characteristics Summary (Jan. 25, 1950)

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