ЦЭЗ ВВС: Старт-2
CEZ VVS: Start-2

General data

Producer info

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Names and dates
Market original model designation
Старт-2
Market model designation (english translation or spelling)
Start-2
Date of prototype completion
1969
People involved
Y. Starinin {Ю. Старинин}Constructor
Config info
Rotorcraft typeAutogyro
Weights
Maximum Takeoff Weight (MTOW)
100
kg
Manufacturers empty weight (MEW)
20
kg
Cabin and cockpit
Maximum number of people onboard
1
Main rotor
Cyclic control
Tilting rotor shaft
Collective control
Yes
Main rotor diameter
4.50
m
Prerotation
Yes
Prerotation type
Solid-fuel rockets
Number of blades
2
Propeller
Mode
Pushing
Propeller diameter
0.80
m
Thrust
294
N
Powerplant
Engine model
Урал
Engine model (english translation or spelling)
Ural
Engine type
Piston
Number of engines
1
Total maximum power
7.50
HP
Static thrust
98
N
Performance
Jump take-off availability
Yes
Heigh achieved during jump take-off
1000
m
0.1007