И. С. Семёнов: СЕМ-1
I. S. Semenov: SEM-1

General data

Producer info

Pictures

Video clips

Data sources

Names and dates
Market original model designation
СЕМ-1
Market model designation (english translation or spelling)
SEM-1
Project start date
1962
Date of prototype completion
1963
Country of manufacture
Russia
People involved
I. Semenov {И. Семёнов}Constructor
Config info
Rotorcraft typeHelicopter
Weights
Maximum Takeoff Weight (MTOW)
450
kg
Cabin and cockpit
Maximum number of people onboard
1
External dimensions
Fuselage length
3.80
m
Main rotor
Drive type
Tip jets
Main rotor diameter
8
m
Powerplant
Engine type
Pulse-jet
Number of engines
2
Performance
Maximum horizontal flight speed (Vh)
150
km/h
0.09