Вертолёт: ВТ-01
Vertolet: VT-01

General data

Producer info

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Data sources

Names and dates
Market original model designation
ВТ-01
Market model designation (english translation or spelling)
VT-01
Date of prototype completion
1993
First flight date and time
1994-02
Country of manufacture
Ukraine
People involved
Vladimir Yakovenko {Владимир Яковенко}Chief design engineer
Evgeny Nechaev {Евгений Нечаев}Test pilot
Config info
Rotorcraft typeHelicopter
Config
Single rotor
Weights
Maximum Takeoff Weight (MTOW)
650
kg
Manufacturers empty weight (MEW)
450
kg
Cabin and cockpit
Maximum number of people onboard
2
Powerplant
Engine model
AI-8
Engine type
Turboshaft
Performance
Cruise speed (Vc)
120
km/h
Maximum service ceiling
1200
m
Maximum range
300
km
0.0495