Myasishchev M-101T
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(Redirected from Myasishchev M-101T Gzhel)
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| M-101T | |
|---|---|
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| An M-101T at 2007 MAKS Airshow | |
| Role | Passenger and cargo aircraft |
| National origin | Russia |
| Manufacturer | Myasishchev |
| First flight | 31 March 1995 |
The Myasishchev M-101T is a Russian business class aircraft, designed by Myasishchev and built by Sokol. The aircraft was first flown on 31 March 1995.[1]
Contents |
[edit] Operators
[edit] Specifications
Data from Brassey's World Aircraft & Systems Directory 1999/2000 [1]
General characteristics
- Crew: 1
- Capacity: 7 passengers
- Payload: 540 kg (1,190 lb)
- Length: 9.975 m (32 ft 9 in)
- Wingspan: 13.0 m (42 ft 8 in)
- Height: 3.72 m (12 ft 2½ in)
- Wing area: 17.06 m² (183.6 sq ft)
- Aspect ratio: 9.906
- Empty weight: 2,016 kg (4,445 lb)
- Max. takeoff weight: 3,000 kg (6,614 lb)
- Powerplant: 1 × Walter M601F turboprop, 567 kW (760 shp) (take-off power)
Performance
- Maximum speed: 525 km/h (283 knots, 326 mph)
- Cruise speed: 360-450 km/h (194-243 knots, 224-280 mph)
- Stall speed: 112-125 km/h (61-68 knots, 90-93 mph)
- Range: 1,410 km (761 nmi, 876 mi)
- Service ceiling: 7,600 m (24,900 ft) (Cruise altitude)
- Climb to 7,600 m (24,900 ft): 25 minutes
[edit] See also
- Aircraft of comparable role, configuration and era
[edit] References
- Taylor, Michael J.H. Brassey's World Aircraft & Systems Directory 1999/2000. London:Brassey's, 1999. ISBN 1 85723 254 7.
[edit] External links
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