Стафийчук А. М.: СА-1
Stafiychuk A. M.: SA-1

General data

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Names and dates
Market original model designation
СА-1
Market model designation (english translation or spelling)
SA-1
Project start date
2000
Country of manufacture
Ukraine
People involved
Anatoly Stafiychuk {Анатолий Стафийчук}Constructor, Test pilot
Config info
Rotorcraft typeHelicopter
Weights
Maximum Takeoff Weight (MTOW)
250
kg
Manufacturers empty weight (MEW)
165
kg
Main rotor
Main rotor diameter
6.05
m
Main rotor blade chord
0.15
m
Tail rotor
Tail rotor diameter
1.20
m
Tail rotor blade chord
0.08
m
Powerplant
Engine model
Suzuki G-10
Engine model (english translation or spelling)
Suzuki G-10
Engine type
Piston
Number of engines
1
Total maximum power
50
HP
Angular speed at max power
5500
rpm
Fuel system
Fuel tank capacity
8
l
Performance
Maximum horizontal flight speed (Vh)
120
km/h
Best rate of climb
5
m/s
Maximum service ceiling
2000
m
Maximum flight endurance
1
h
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