Папст А. В.
Papst A. V.

General data

Producer info

Pictures

Video clips

Data sources

Names and dates
Approximated date of prototype completion
Early 1990's
Country of manufacture
Kazakhstan
People involved
Alexander Papst {Александр Папст}Constructor
Config info
Rotorcraft typeHelicopter
Config
Coaxial rotors
Weights
Maximum Takeoff Weight (MTOW)
360
kg
Manufacturers empty weight (MEW)
180
kg
Cabin and cockpit
Maximum number of people onboard
2
Main rotor
Collective control
Yes
Main rotor diameter (System no.: 1)
6.40
m
Main rotor diameter (System no.: 2)
6.40
m
Powerplant
Engine model
Volkswagen
Total maximum power
75
HP
Performance
Cruise speed (Vc)
90
km/h
0.0951