Ace K-1

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The Ace K-1 was a single-seat biplane designed in 1919 by Alexander Klemin, then Professor of Aeronautical Engineering at New York University (NYU). Later versions included a nearly faired-in engine installation and some were fitted with the Salmson AD-9 engine.

Contents

[edit] Specifications (K-1)

[edit] General characteristics

  • Crew: one pilot
  • Capacity: pilot only
  • Length: 18 ft 0 in (5.49 m)
  • Wingspan: 28 ft 4 in (8.64 m)
  • Height: ft in ( m)
  • Wing area: ft² ( m²)
  • Empty: lb ( kg)
  • Loaded: lb ( kg)
  • Maximum takeoff: lb ( kg)
  • Powerplant: 40 hp (36 kW) inline

[edit] Performance

  • Maximum speed: 63 mph (100 km/h)
  • Range: 160 miles (256 km)
  • Service ceiling: ft ( m)
  • Rate of climb: ft/min ( m/min)
  • Wing loading:
  • Power/Mass:

[edit] Related content

Related development:

Comparable aircraft:

Designation sequence: