Aero A.17

The Aero A.17 was a small sailplane built in Czechoslovakia in 1922. The conventional sailplane wing and tail were held together by an open truss framework, which also supported the pilot.

Specifications (Aero A.17)

General Characteristics

  • Crew: one, pilot
  • Length: 4.34 m (14 ft 3 in)
  • Wingspan: 13.80 m (45 ft 3 in)
  • Height: m ( ft in)
  • Wing area: 15.9 m² (171 ft²)
  • Aspect ratio: 1:11.4
  • Empty: 47 kg (103 lb)
  • Loaded: 127 kg (279 lb)
  • Maximum takeoff: kg ( lb)

Performance

  • Maximum speed: km/h ( mph)
  • Maximum glide ratio:
  • Rate of sink: m/min ( ft/min)
  • Wing loading: 8 kg/m² (1.6 lb/ft²)

Related Content

Related development: Comparable aircraft: Stamer Zgling Designation sequence: A.12 - A.14 - A.15 - A.17 - A.18 - A.19 - A.20

 

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