Technical data | |
---|---|
Type | Su-1 |
Function | Fighter |
Year | 1940 |
Crew | 1 |
Engines | 1*1100hp M-105P |
Length | 8.42m |
Wingspan | 11.5m |
Wing area | 19.0m2 |
Empty weight | 2495kg |
Loaded weight | 2875kg |
Wing Load (kg/m2) | 151 |
Power load (kg/hp) | 2.6 |
Speed at 0m | 500km/h |
Speed at 10000m | 641km/h |
Ceiling | 12500m |
Climb | |
5000m | 4.9min |
Range | 720km |
Armament | |
Cannon | 1*20mm ShVAK |
M-Guns | 2*7.62mm ShKAS |
![]() |
Specialized high-altitude interceptor. Standard armament for pre-WWII fighter with liquid cooled engine: cannon firing through the propeller shaft and pair of synchronized machineguns. Fuselage was made of wood, wings - duralumin. Main landing gear - retractable backwards with 90° turn, tailwheel also retractable.
Aircraft was flown since August 1940. It performed very well, but TK-2 turbochargers were faulty and failed to deliver before the German invasion.
Turbochargers problems and bureau evacuation resulted in cancellation of the Su-1.
One built.
![]() I-360/Su-3; |
Modified November 31, 1997 | ![]() |
Back to Main Gate |