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 Accepted | 2 |
| RDT&E Costs | $5.1 million |
| F-90 | |
| Year deployed | |
| Wing span, m | 12.19 |
| Length, m | 17.17 |
| Height, m | 4.80 |
| Wings area, m2 | 32.05 |
| Weight, kg | |
| - empty aircraft | 8401 |
| - normal take-off | 10152 |
| - 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, km | 3700 |
| Rate of climb, m/min | - |
| Service ceiling, m | 11900 |
| Crew | 1 |
| Armament |
|
|
NEWSLETTER
|
| Join the GlobalSecurity.org mailing list |
|
|
|
