Tupolev Tu-22M

Length
42.46 m
Flat Wing Span
34.28 m
Height
11.05 m
Flat Wing Area
183.6 m²
Max Speed
1997 km/h
Max Mach
1.88 Mach
Max Ceiling
13300 m
Number of Engines
2
Aircraft Engine
First Flight
1969-08-30
Entry Into service
1972-01-01
Number Built
497
Maximum Take-Off Weight
126 t (paragliders: kg)
Maximum Range
6800 km

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Aircraft Weight Variants

Aircraft Maximum Take-Off Weight (t (paragliders: kg)) Maximum Range (km)
Tupolev Tu-22M 126 6800

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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