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North American T-39A


General information


ManufacturerNorth American
ModelT-39 Sabreliner
ModificationT-39A
CountryUSA
Years1958
TypeOther
Main rotor diameter-
Tail rotor diameter-
Wingspan13.56 m
Length13.41 m
Height4.88 m
Wing area34.70 m2
Zero fuel weight-
Empty weight5980 kg
Maximum takeoff weight8459 kg
Normal takeoff weight-
Flight duration-
Engine2 ТРД Pratt Whitney J-60
Power-
Thrust2 x 1360 kN
Maximum speed866 km/h
Cruising speed805 km/h
Rate of climb-
Practical range2740 km
Service ceiling9120 m
Hovering ceiling-
Crew2