Entry Into service
1972-01-01
Maximum Take-Off Weight
126 t (paragliders: kg)
Pictures
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Aircraft Weight Variants
| Aircraft |
Maximum Take-Off Weight (t (paragliders: kg)) |
Maximum Range (km) |
|
Tupolev Tu-22M |
126 |
6800 |
Similar airplanes
All data (28 fields)
- Name
- Tupolev Tu-22M
- Manufacturer
- Tupolev
- Description
- The Tupolev Tu-22M (; NATO reporting name: Backfire) is a Soviet nuclear capable, supersonic, variable-sweep wing, long-range strategic and maritime strike bomber developed by the Tupolev Design Bureau in the 1960s.
- ICAO Code
- T22M
- First Flight
- 1969-08-30
- Entry Into service
- 1972-01-01
- Production End
- 1993-01-01
- Designer
- Tupolev
- Type
- Strategic bomber/Maritime strike
- Length (m)
- 42.46
- Height (m)
- 11.05
- Cockpit Crew
- 4
- Max Speed (km/h)
- 1997
- Max Ceiling (m)
- 13300
- Rate of Climb (m/s)
- 15
- Armament
- 1 × 23-mm GSh-23 cannon in remotely controlled tail turret; wing and fuselage pylons and internal weapons bay
- Max Mach (Mach)
- 1.88
- National Origin
- Soviet Union
- Number Built
- 497
- Powerplant Description
- 2 × Kuznetsov NK-25 Afterburning turbofan engines
- Primary Users
- Russian Aerospace Forces, Soviet Air Forces (historical), Ukrainian Air Force (historical)
- Status
- In service
- Wikipedia Article (URL)
- en.wikipedia.org/wiki/Tupolev_Tu-22M
- Flat Wing Span (m)
- 34.28
- Flat Wing Area (m²)
- 183.6
- Wake Category
- M
- Aircraft Engine
- Kuznetsov NK-25
- Number of Engines
- 2