Tu-91 made its first flight on 2 November 1954.
Crew: Two (Pilot and Observer)
Length: m
Wingspan: m
Height: m
Wing area: 47.5 m²
Empty weight: 8,000 kg
Max. takeoff weight: 14,400 kg
Powerplant: 1 × Isotov TV2M turboprop, 5,709 kW
Maximum speed: 800 km/h (flight-tested to speeds as fast as 760 km/h and altitudes as high as 6500m)
Cruise speed: 250-300 km/h
Range: 2,350 km
Service ceiling: 11,000 m
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