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Military


XF-90

Specifications
Length/Span 56.2/39.2 ft
Loaded Weight 26,900 lbs.
Engine, Number & Designation 2J-34-WE-11/22
Max Speed 616.5 knots
Crew 1
Initial Contract Date 20 June 1946
First Flight (experimental) 4 June 1949
Quantity Ordered 2
Total Accepted2
RDT&E Costs $5.1 million



F-90
Year deployed
Wing span, m 12.19
Length, m 17.17
Height, m4.80
Wings area, m2 32.05
Weight, kg
- empty aircraft8401
- normal take-off10152
- maximum take-off 12340
Engine 2 Westinghouse J34-WE-15
Thrust dry, kN 2 x 1905
Maximum speed, km/h 1070
Cruising speed, km/h 798
Range, km3700
Rate of climb, m/min-
Service ceiling, m11900
Crew1
Armament
  • 6 20-mm cannons
  • Bombs - 746 kg
  • Light bombs or 8 127-mm UR HVAR.


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