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

Su-1 / I-330, P.O.Sukhoj

32k b/w photo from "History of aircraft construction in the USSR", Vol.2 p.49;

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.



Developments/Modifications(s):

I-360/Su-3
;



References:
  • "History of aircraft construction in the USSR", Vol.2 p.48-49;


  • More Links...
  • Su-1 (I-330)
  • I-330, Sukhoi
  • Su-1, Sukhoi

  • Modified November 31, 1997 Back to
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