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General information


ManufacturerInstytut Lotnictwa
ModelLala-1
ModificationLala-1
CountryPoland
Years1972
TypeExperimental aircraft
Main rotor diameter-
Tail rotor diameter-
Wingspan18.20 m
Length12.40 m
Height4.00 m
Wing area-
Zero fuel weight-
Empty weight4440 kg
Maximum takeoff weight5500 kg
Normal takeoff weight-
Flight duration-
Engine1 PZL Kalisz ASh-62IR+ 1 ТРД АИ-25
Power1 x 1000 + 1x 1500 HP
Thrust-
Maximum speed200 km/h
Cruising speed-
Rate of climb-
Practical range180 km
Service ceiling7000 m
Hovering ceiling-
Crew2
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