Myasishchev M-101T Gzhel
From Wikipedia, the free encyclopedia
The Myasishchev M-101T Gzhel is a Russian business class aircraft, designed by Myasishchev and built by Sokol.
The aircraft was first flown on the 31 March 1995.
Contents |
[edit] Operators
[edit] Specifications
[edit] General characteristics
- Crew:
- Capacity: 7 passengers
- Length: ft 7in ( m)
- Wingspan: ft in ( m)
- Height: ft in ( m)
- Wing area: ft² ( m²)
- Empty: lb ( kg)
- Loaded: lb ( kg)
- Maximum takeoff: lb ( kg)
- Powerplant: Walter M-601, 760hp (565kW)
[edit] Performance
- Maximum speed: mph ( km/h)
- Range: miles ( km)
- Cruise: mph
- Service ceiling: ft ( m)
- Rate of climb: ft/min ( m/minmpm)
- Wing loading: lb/ft² ( kg/m²)
- Power/mass: hp/lb ( kW/kg)
[edit] References
http://www.flightglobal.com/articles/2003/06/10/166548/class-struggle.html
|