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XFV-12 | ||
Experimental fighter with VTOL | ||
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Specification: | |
Wing span, m
Lenght, m Height, m Wings area, m2 Weight, kg - empty operating - normal take-off - maximum take-off VTOL - maximum take-off STOL Internal fuel, l Engine Thrust, kgs - normal - at take-off Maximum speed, km/h Range, km Service ceiling, m Crew |
- 8.69 - 13.39 - 3.15 - 27.20 - 6259 - 8845 - 11000 - 12300 - 2763 - 1 TJE Pratt & Whitney F401-PW-40 - 1 X 62.56 - 1 X 96.99 - 2200 - - - 1 |