Flat Wing Aspect Ratio
10.6
Maximum Take-Off Weight
23.8 t (paragliders: kg)
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Aircraft Weight Variants
| Aircraft |
Maximum Take-Off Weight (t (paragliders: kg)) |
Maximum Range (km) |
|
Myasishchev M-55 |
23.8 |
4965 |
Similar airplanes
All data (21 fields)
- Name
- Myasishchev M-55
- Manufacturer
- 1940-1960
- Description
- The Myasishchev M-55 (NATO reporting name: Mystic-B) is a high-altitude reconnaissance aircraft developed by OKB Myasishchev in the Soviet Union, similar in mission to the Lockheed U-2, but with a twin-boom fuselage and tail surface design.
- First Flight
- 1978-12-01
- Designer
- 1940-1960
- Type
- High-altitude reconnaissance
- Length (m)
- 22.867
- Height (m)
- 4.8
- Cockpit Crew
- 1
- Max Ceiling (m)
- 21500
- Endurance (h)
- 6.5
- Number Built
- 34
- Powerplant Description
- 2 × Soloviev D-30-V12 low-bypass turbofan, 93.19 kN thrust each
- Primary Users
- Soviet Air Force, Russian Aerospace Forces
- Status
- Potentially returning to service
- Wikipedia Article (URL)
- en.wikipedia.org/wiki/Myasishchev_M-55
- Flat Wing Span (m)
- 37.46
- Flat Wing Area (m²)
- 131.6
- Flat Wing Aspect Ratio
- 10.6
- Aircraft Engine
- Soloviev D-30
- Number of Engines
- 2