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Specification Tu-22KD 'Blinder-C'
Powerplant: two 156.9 kN (35,275 lb st) VD-7M afterburning turbojets; later
two 161.9 kN (36,376 lb st) RD-7M2 afterburning turbojets
Dimensions: length 42.60m (139 ft 9 in); height 10.00m (32 ft 9¼ in);
wing span 23.50m (77 ft 1¼ in)
Weights: empty 40000 kg (88,183 lb); Max Take-Off Weight 84000 kg (185,185 lb) or 94000 kg (202,820 lb)
with four take off rockets
Performance: max level speed at 12200 m (40,000 feet) Mach 1.5 or 1510 km/h (938 mph);
max level speed at sea level 890 km/h (553 mph);
ceiling 18300m (60,040 ft)
Armament:
two R-23 23mm cannons in the tail for self-defence;
up to 24000 kg (847,547 lb) bomb load consisting of either one Kh-22 (conventional) or one Kh-22N (nuclear warhead) anti-ship missile
carried on its belly semi lowered into the weapons bay,
or up to 24 FAB-500 500kg freefall bombs or one FAB-9000 9000 kg freefall bomb carried in the internal weapons bay.
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Tu-22 pilot instrument panel
Tu-22 weapons officer panel
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