Aerocar IMP
 | This article needs additional citations for verification. (December 2009) |
| Aerocar IMP | |
|---|---|
| General information | |
| Type | Light aircraft |
| National origin | United States |
| Manufacturer | Aerocar International |
| Designer | |
| Status | Abandoned project |
The Aerocar IMP (for Independently Made Plane) was an unconventional light aircraft designed by Moulton Taylor[1] and marketed for homebuilding. The IMP and its various derivatives were developed by Taylor's Aerocar business after he had already established himself in the homebuilt market with the Coot amphibian, and at the time of the energy crisis in the United States, were designed to be economical to build and operate.
The IMP was unconventional in configuration in having a pusher propeller powered by a long driveshaft from an engine mounted midway within the fuselage of the aircraft. This provided an aerodynamic advantage over more traditional pusher arrangements by allowing greater streamlining of the fuselage – giving the IMP the appearance of an elongated teardrop. The aircraft's most visually striking feature, however, is its inverted V-tail.
Originally designed as a four-seat aircraft, the original IMP design proved to be too complex and expensive for the market that Taylor was aiming for, and although it was awarded a type certification by the FAA, development was abandoned in favour of scaled-down, single-seat version dubbed the Mini-IMP.
Specifications (IMP)
[edit]General characteristics
[edit]- Crew: one pilot
- Capacity: 3 passengers
- Length: 22 ft 0 in (6.70 m)
- Wingspan: 29 ft 0 in (8.84 m)
- Height: ft in ( m)
- Wing area: 112 ft2 ( 10.39 m2)
- Empty: 950 lb (430 kg)
- Loaded: 1550 lb (703 kg)
- Maximum takeoff: lb ( kg)
- Powerplant: 1x Franklin 4R, 200 hp (149 kW)
Performance
[edit]- Maximum speed: 150 mph (240 km/h)
- Range: miles ( km)
- Service ceiling: ft ( m)
- Rate of climb: 800 ft/min ( m/min)
- Wing loading: 13.8 lb/ft2 ( kg/m2)
- Power/Mass: 0.1290 hp/lb (0.04966 kW/kg)
- Propeller diameter: 6 ft (1.82 m)[2]
See also
[edit]Related development
References
[edit]
- ^ "Aerocar performance and specifications". Pilot Friend. Retrieved 10 April 2017.
- ^ Crawford, Donald R. (1994). A practical guide to airplane performance and design (3rd print., rev. ed.). Torrance, Ca: Crawford Aviation. ISBN 0-9603934-0-4.