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.
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[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:
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