Myasishchev M-101T Gzhel

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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

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[edit] Specifications

[edit] General characteristics

  • Crew:
  • Capacity: 7 passengers
  • Length: ft 7in ( m)
  • Wingspan: ft in ( m)
  • Height: ft in ( m)
  • Wing area: ft² ( m&sup2)
  • 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

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