Technical data
Type P-1
Function fighter
Year 1958
Crew 2
Engines 1*10600kg Lyulka AL-7F
Speed 2050km/h
Ceiling 19500m
Range 2000km
Armament 50*rockets 57mm

P-1, P.O.Sukhoj


Experimental fighter. The P-1 was a tailed two-seat delta. It had oval jet intakes just ahead of the wing root, with twin shock cones. Armament was retractable rocket launchers in the nose, behind the radar. The big P-1 was underpowered (??) with the single Lyulka AL-7F engine.

No production.


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