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Yakovlev AIR-1

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AG/1 for engines. Yakovlev designed his first aircraft while working at the Zhukovsky Military Aviation Academy; the aircraft was a two-seat light biplane powered by a 60 hp (45 kW) ADC Cirrus piston engine.[1] Although the directors of the Academy were opposed to the design, the aircraft was built in the Academy Club on his own time.[2] Originally designated VVA-3 (Military Aviation Academy-3) Yakovlev later redesignated it the AIR-1 in honour of Alexei Ivanovich Rykov, the country's premier (the Chairman of the Council of People's Commissars) and the president of the Osoviakihm.[2] The first flight on 12 May 1927 was flown by Yakovlev's friend J.I. Piontkovsky, who later rated the flying qualities as excellent; Piontkovsky later flew the aircraft non-stop from Sevastopol to Moscow in 15½ hours, a distance of 1240 km.[2] In 1928 Yakovlev produced an improved variant, the AIR-2; six were built between 1928 and 1931 fitted with different five-cylinder radial engines.[2] One aircraft powered by a Siemens engine was designated AIR-2S and was fitted with floats designed by V B Shavrov. (from wikipedia)

General Characteristics

  • Created On Windows
  • Wingspan 49.9ft (15.2m)
  • Length 37.6ft (11.4m)
  • Height 13.6ft (4.1m)
  • Empty Weight 8,727lbs (3,958kg)
  • Loaded Weight 9,177lbs (4,162kg)

Performance

  • Horse Power/Weight Ratio 0.108
  • Wing Loading 18.5lbs/ft2 (90.4kg/m2)
  • Wing Area 495.5ft2 (46.0m2)
  • Drag Points 18850

Parts

  • Number of Parts 244
  • Control Surfaces 6
  • Performance Cost 874