Su-7BM

Fighter/bomber

First flight:	on April, 24 1959
Crew:	1 person
Engine:	AL-7F 1-100 by traction 6800(on forcing - 9 600) kgf
Length(with BSA ) :	a 18.583 m
Wingspan:	a 9.309 m
An wing area covered:	34.0 m2
Flight weight:	normal is 11 983 kg, maximal is 13 043 kg
High speed:	2120 km/h(M=2)
Practical ceiling:	a 19 500 m
Distance of flight :	1130 kilometres
Running approach/is a run:	a 1350/900 m
Armament:	two 30-мм cannons of НР-30(ammunition - for 80 projectiles), НАР, bomb and RBC by gross weight to 2000 kg
Mass production:	1960-62 Only in 1957-72 it was built 1847 airplanes of type of SU-7 all models, from them on an export(in 9 countries) – 691 airplanes.

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