АэроПромСервис: DOPPLER 001
AeroPromService: DOPPLER 001

General data

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Names and dates
Market original model designation
DOPPLER 001
Market model designation (english translation or spelling)
DOPPLER 001
Approximated date of prototype completion
Early 2000's
First flight date and time
2002
People involved
Alexander Rusak {Александр Русак}Chief design engineer
Config info
Rotorcraft typeAutogyro
Weights
Maximum Takeoff Weight (MTOW)
500
kg
Manufacturers empty weight (MEW)
260
kg
Main rotor
Main rotor diameter
8.54
m
Prerotation
Yes
Prerotation type
Hydraulic
Powerplant
Engine model
BMW
Engine model (english translation or spelling)
BMW
Number of engines
1
Total maximum power
100
HP
Fuel system
Fuel tank capacity
40
l
Average fuel consumption [volumetric]
12
l/h
(...)
9
l/h
Performance
Maximum horizontal flight speed (Vh)
150
km/h
Minimum speed
35
km/h
Take-off distance
80
m
(...)
10
m
Landing distance
5
m
(...)
0
m
Maximum range
600
km
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