Sponsored ads


Start | Leduc | Leduc 0.20(0.21-0.22)


General information


ManufacturerLeduc
ModelLeduc 0.20(0.21-0.22)
ModificationLeduc 0.22
CountryFrance
Years1956
TypeExperimental aircraft
Main rotor diameter-
Tail rotor diameter-
Wingspan10.00 m
Length17.00 m
Height4.50 m
Wing area22.40 m2
Zero fuel weight-
Empty weight6000 kg
Maximum takeoff weight-
Normal takeoff weight11000 kg
Flight duration0.15-1 h
Engine1 SNECMA Atar 1010-3
Power-
Thrust1 x 26.47 kN
Maximum speed4000 km/h
Cruising speed-
Rate of climb-
Practical range-
Service ceiling25000 m
Hovering ceiling-
Crew1
Sponsored ads