Technical data
Type I-305/FL
Function Fighter, Experimental
Year 1947
Crew 1
Engines 1*1500kg TR-1A
Length 9.816m
Wingspan 10.0m
Wing area 18.2m2
Empty weight 3055kg
Loaded weight 4570kg
Wing Load (kg/m2) 251
Power load (kg/hp) 3.05kg/kgf
Speed at 0m 898km/h (expected)
Speed at 5000m 885km/h (expected)
Landing Speed 155km/h (expected)
Turn time 25.9 sec (expected)
Range 1050km (expected)
Ceiling 13400m (expected)
Climb
5000m 4.86 min (expected)
10000m 13.24 min (expected)
Armament
Guns 1*g37mm NS-37
2*g23mm NS-23

I-305, FL by A.I.Mikoyan/M.I.Gurevich


Version of the MiG-9 with single 1350kg A.M.Lyulka TR-1A engine.

One was built in Fall 1946. It was not flown because engines systematically failed during bench tests, and designers were under strong pressure of getting the standard twin-engined MiG-9 into full-scale production.


ReferencesLinks
  • "History of aircraft construction in the USSR", Vol.1 p.341-342;
  • "OKB MiG - a history of the design bureau and its aircraft" by Piotr Butowski and Jay Miller, pp58-59;
  • I-305, Mikoyan-Gurevich

  • Created October 23, 1997
    Modified November 4, 1998;
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