Engineering:Grigorovich MU-2
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Revision as of 19:36, 18 June 2021 by imported>AstroAI (over-write)
Grigorovich MU-2 | |
---|---|
Role | Trainer flying boat |
Manufacturer | Grigorovich |
First flight | 1928 |
Number built | 1 |
The Grigorovich MU-2 was a trainer flying boat built in the Soviet Union in the mid-1920s. It was designed by the Grigorovich Design Bureau after the failure of the Grigorovich MUR-1, featuring an all-metal hull. However, it was never put into production due to poor performance and sluggish take-off behavior.[1]
Specifications
Data from [1]
General characteristics
- Crew: two
- Length: 8.6 m (28 ft 3 in)
- Wingspan: 11.8 m (38 ft 9 in)
- Wing area: 35.6 m2 (383 sq ft)
- Empty weight: 820 kg (1,808 lb)
- Gross weight: 1,086 kg (2,394 lb)
- Powerplant: 1 × Shvetsov M-11 five-cylinder air-cooled radial, 75 kW (100 hp)
Performance
- Maximum speed: 136 km/h (85 mph, 73 kn) at sea level 136 km/h (85 mph; 73 kn) at 0 m (0 ft)
- Range: 380 km (240 mi, 210 nmi)
- Endurance: 3 hours
- Service ceiling: 3,150 m (10,330 ft)
- Time to altitude: 1,000 m (3,300 ft) 10.8 minutes
- Wing loading: 30.9 kg/m2 (6.3 lb/sq ft)
References
- ↑ 1.0 1.1 "MU-2 by D.P.Grigorovich". Ram-home.com. 1998-07-29. http://ram-home.com/ram-old/mu-2.html. Retrieved 2019-12-19.
Bibliography
- Shavrov, V. B. (1985) (in Russian). Moscow: Машиностроение. pp. Vol 1 pp.401-402.
- Kulikov, Victor (December 1996). "Le fascinante histoire des hydravions de Dimitry Grigorovitch" (in French). Avions: Toute l'aéronautique et son histoire (45): 20–33. ISSN 1243-8650.
![]() | Original source: https://en.wikipedia.org/wiki/Grigorovich MU-2.
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