Dobiáš P.
Dobias P.

General data

Producer info

Pictures

Video clips

Data sources

Names and dates
Date of prototype completion
1973
Country of manufacture
Czech Republic
People involved
Petr Dobias {Petr Dobiáš}Constructor
Config info
Rotorcraft typeGyroglider
Weights
Maximum Takeoff Weight (MTOW)
260
kg
Manufacturers empty weight (MEW)
77
kg
Cabin and cockpit
Maximum number of people onboard
2
External dimensions
Length
3.46
m
Main rotor
Main rotor diameter
6.82
m
Performance
Towed speed
60
km/h
Landing speed
30
km/h
0.0445