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Tupolev Tu-22M ✕ Tupolev Tu-104 ✕
Manufacturer Tupolev 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. The Tupolev Tu-104 (NATO reporting name: Camel) is a medium-range, narrow-body, twin turbojet-powered Soviet airliner.
ICAO Code T22M
First Flight 1969-08-30 1955-06-17
Entry Into service 1972-01-01 1956-09-15
Production End 1993-01-01 1960-01-01
Service End 1981-01-01
Designer Tupolev Andrei Tupolev
Type Strategic bomber/Maritime strike Narrow-body jetliner
Length (m) 42.46 40.06
Height (m) 11.05 11.9
Cockpit Crew 4 7
Max Seating 115
Max Speed (km/h) 1997 950
Max Ceiling (m) 13300 12000
Rate of Climb (m/s) 15 10
Armament 1 × 23-mm GSh-23 cannon in remotely controlled tail turret; wing and fuselage pylons and internal weapons bay
Capacity Description 50–115 passengers
Max Mach (Mach) 1.88
National Origin Soviet Union
Number Built 497 201
Powerplant Description 2 × Kuznetsov NK-25 Afterburning turbofan engines 2 × Mikulin AM-3M-500 turbojet engines
Primary Users Russian Aerospace Forces, Soviet Air Forces (historical), Ukrainian Air Force (historical) Aeroflot, ČSA
Status In service Retired
Wikipedia Article (URL) en.wikipedia.org/wiki/Tupolev_Tu-22M en.wikipedia.org/wiki/Tupolev_Tu-104
Flat Wing Span (m) 34.28 34.54
Flat Wing Area (m²) 183.6 183
Wake Category M
Aircraft Engine Kuznetsov NK-25
Number of Engines 2 2