VT-11, N.N.Polikarpov/D.P.Grigorovich

19k b/w photo from the "History of aircraft construction in the USSR" by V.B.Shavrov, Vol.1 p.436

P
rototype of the I-5.
N.N.Polikarpov was assigned to develope the I-6 (primarily wooden) fighter (delivery July/August 1930) under provisions of the Five Year Plane for experimental aircraft design (starting 1928). At the same time D.P.Grigorovich was working on his his own I-5 design, different from Polikarpov's (and Tupolev's I-5).
When the unrealistic Plane was obviously failed, N.N.Polikarpov, D.P.Grigorovich and other ~450 aircraft designers and engineers were arrested by the NKVD as "saboteurs and enemy infiltrators". Some 300 survived, and were arranged to work in the police supervised design bureaus and experimental factories.
Initially working separately, N.N.Polikarpov and D.P.Grigorovich joined their forces and the wooden mock-up was ready on 28 March 1930. The conditions of the enforced labor 'helped' designers and workers to complete the prototype within 30 days after the mock-up. It was designated VT-11, carrying letters "VT" on the rudder. Here VT stays for the "Vnutrennaja Tur'ma", "Internal Prison". Aircraft was test-flown on April 29, 1930 by test-pilot Benedict Bukholz.
One month later the second prototype "Klim Voroshilov" was completed. They had different engines (so different cowling design) and some other minor changes were introduced. Those two prototypes had individual fairings covering cylinder heads.
Third prototype ("Present to the XVI Party Congress") was powered with domestic high-altitude M-15 engine. It differed from other two by NACA cowling, covering whole engine.
All prototypes were highly praised by test-pilots for their exceptional handling characteristics. Stalin was provided with the fighter he wanted. The design team was released from prison, and soon N.N.Polikarpov was crowned as a "King of Fighters". Not all designers and engineers shared this luck, and about 150 vanished in Stalin's camps and prisons.
Seven pre-production VT-11 were built, nearly identical to the second prototype. Small headrest fairing was added, main wheel shock were uncovered. No serious complications were revealed, and aircraft went into production as I-5;
Sources :
  • "History of aircraft construction in the USSR" by V.B.Shavrov, Vol.1 p.435-438
  • 'Polikarpov Fighters in action, Part 1' by Hans-Herri Stapfer.
    More links...
  • VT-11, Polikarpov
  • VT-12, Polikarpov
  • VT-13, Polikarpov
  • Technical data
    Type VT-11 "Klim Voroshilov" "Present to the XVI Party Congress"
    Function fighter prototype
    Year 1930
    Crew 1
    Engine 1*450hp Bristol Jupiter VII 1*420/525hp Bristol Jupiter VI 1*450hp M-15
    Length 6.78m 6.78m 6.80m
    Wingspan 10.2m
    Wing area 21.25m2
    Empty Weight 919kg 924kg 948kg
    Maximum Weight 1331kg 1336kg 1360kg
    Wing load 62.4kg/m2 62.5kg/m2 63.8kg/m2
    Power load 2.9kg/hp 2.9kg/hp 3.1kg/hp
    Speed at 0m 238km/h 267km/h 260km/h
    Speed at 3000m 273km/h 264km/h 259km/h
    Landing Speed 95km/h
    3600 turn 14sec 16sec 11sec
    Range 700km 650km 620km
    Ceiling 7800m 7600m 8200m
    Climb
    1000m 1.4min 1.4min 1.5min
    2000m 2.8min 3.1min 3.3min
    3000m 4.8min 5.1min 5.6min
    5000m 9.2min 9.6min 10.0min
    Modified May 19, 1997
    by Alexandre Savine;
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