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Polikarpov I-6

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I-6
Role Fighter
National origin Soviet Union
Manufacturer Polikarpov
Designer Nikolai Polikarpov
First flight 30 March 1930
Status prototype
Number built 2

The Polikarpov I-6 was a Soviet biplane fighter prototype of the late 1920s. It was designed with traditional wooden construction in comparison with the wood and steel tube construction Polikarpov I-5. Its development took longer than planned and the lead designer, Nikolai Polikarpov, was arrested for industrial sabotage, which only further delayed the project. Only two prototypes were built, as the I-5 was selected for production.

Design and development

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Development of the I-6 (Istrebitel'—fighter) began in September 1928 with a deadline for delivery for the first prototype of 1 August 1929 after the first prototypes of the Polikarpov I-3 were completed. Although the new fighter shared many of the characteristics of the earlier design, including the staggered sesquiplane, single-bay, layout of the wings, it was a new design which used a nine-cylinder, single-row, air-cooled Bristol Jupiter radial engine rather the water-cooled inline engine of its predecessor. It was designed by the OSS (Russian: Otdel Sookhoputnykh Samolyotov—Landplane Department), later redesignated as OPO-1 (Russian: Opytnyy Otdel—Experimental Department) of Aviatrest ("Aviation Trust") under the supervision of Nikolai Polikarpov, head designer of the department. It was originally intended to be compared to the I-3, but this was changed to an evaluation of construction methods with the wooden construction I-6 compared to the mixed construction Polikarpov I-5. Both aircraft used the Jupiter VI engine for which a license had recently been negotiated.[1]

The I-6 had an oval-section semi-monocoque fuselage covered with 'shpon', molded birch plywood, with a small headrest faired into the fuselage, although the engine was enclosed in a metal cowling that left the cylinder heads exposed for better cooling. The two-spar wings were covered in plywood and fabric and had a Clark Y profile. Internal bracing wires were fitted to reinforce the wings. The control surfaces were framed in duralumin, but covered in fabric. The duralumin N-type struts that separated the wings, and attached the upper wing to the fuselage, had a teardrop profile. They were reinforced with steel bracing wires. The conventional undercarriage was fixed with rubber shock absorbers. The wooden propeller was given a spinner.[2] The lighter weight of the air-cooled Jupiter engine, which required neither a heavy radiator nor coolant, meant that the I-6 had an empty weight only 62% of that of the I-3.[1]

Polikarpov was arrested and imprisoned by the OGPU in September 1929 for the crime of industrial sabotage when neither the I-6 nor the I-5 projects met their stipulated deadlines,[3] and this delayed the first flight of the I-6 until 30 March 1930. The second prototype was completed shortly thereafter and both aircraft appeared in that year's May Day fly-past over Moscow. Both aircraft likely used imported engines before they were replaced by the Soviet-built copy of the Jupiter, the Shvetsov M-22. One I-6 crashed on 13 June 1930 after the test pilot bailed out, without justification, in the opinion of the Soviet aviation historian Vadim B. Shavrov.[1]

The I-5 and the I-6 were virtually identical in performance, although the I-6 took 15 seconds to complete a full circle versus the 9.5 seconds of the I-5. Both aircraft were armed with two 7.62 mm (0.3 in) PV-1 machine guns, but the production model of the I-5 was expected to be armed with four, although this proved to impose too great a penalty to the I-5's performance. The exact reasons for the selection of the I-5 over the I-6, which was debated for a full year, are not known, but likely relate to both of these factors. Curiously, Polikarpov was not informed of the selection of the I-5 until his release in 1933[1] after his initial sentence of death had been commuted to ten years of imprisonment in a labor camp.[4]

Specifications

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Data from Istoriia konstruktskii samoletov v SSSR do 1938 g.[5]

General characteristics

  • Crew: 1
  • Length: 6.8 m (22 ft 4 in)
  • Wingspan: 10 m (32 ft 10 in)
  • Wing area: 20.5 m2 (221 sq ft)
  • Empty weight: 868 kg (1,914 lb)
  • Gross weight: 1,280 kg (2,822 lb)
  • Powerplant: 1 × Shvetsov M-22 9-cylinder air-cooled radial piston engine, 313 kW (420 hp)
  • Propellers: 2-bladed fixed-pitch propeller

Performance

  • Maximum speed: 280 km/h (170 mph, 150 kn)
  • Range: 700 km (430 mi, 380 nmi)
  • Service ceiling: 7,500 m (24,600 ft)
  • Time to altitude: 5,000 m (16,000 ft) in 10 minutes
  • Wing loading: 62 kg/m2 (13 lb/sq ft)
  • Power/mass: 0.245 kW/kg (0.149 hp/lb)
  • Horizontal turn time: 15 sec

Armament

  • Guns: 2 × 7.62  mm (0.30  in) PV-1 machine guns

See also

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Related development

Aircraft of comparable role, configuration, and era

References

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  1. ^ a b c d Gordon and Dexter, p. 11
  2. ^ Gunston, pp. 298–299
  3. ^ Gordon and Dexter, p. 13
  4. ^ Gordon and Dexter, p. 4
  5. ^ Shavrov, V. B. (1985). Istoriia konstruktskii samoletov v SSSR do 1938 g. (3izd.) (in Russian). Mashinostroenie. ISBN 5-217-03112-3.

Bibliography

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  • Gordon, Yefim; Dexter, Keith (2002). Poliarpov's Biplane Fighters. Red Star. Vol. 6. Hinckley, England: Midland Publishing. ISBN 1-85780-141-5.
  • Green, William; Gordon Swanborough. The Complete Book of Fighters. Godalming, UK: Salamander Books. p. 415.
  • Gunston, Bill (1995). The Osprey Encyclopedia of Russian Aircraft 1875-1995. London: Osprey. ISBN 1-85532-405-9.
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