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General information


ManufacturerRockwell, MBB
ModelX-31A
ModificationХ-31А
CountryUSA
Years1990
TypeExperimental aircraft
Main rotor diameter-
Tail rotor diameter-
Wingspan-
Length14.85 m
Height4.44 m
Wing area21.02 m2
Zero fuel weight-
Empty weight-
Maximum takeoff weight7228 kg
Normal takeoff weight6623 kg
Flight duration-
Engine-
Power-
Thrust1 x 71.17 kN
Maximum speed2752 km/h
Cruising speed-
Rate of climb-
Practical range-
Service ceiling12190 m
Hovering ceiling-
Crew1
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