Aerocar Micro-IMP

Aerocar Micro-Imp
Role	Single seat light aircraft
National origin	United States of America
Manufacturer	Aerocar
First flight	1981
Number built	1
Developed from	Aerocar IMP

The Aerocar Micro-IMP was a light sportsplane developed from the successful Mini-IMP homebuilt. Designed by Moulton Taylor and Jerry Holcomb in 1978, it was finished in 1981 and demonstrated at Oshkosh the following year.

A unique feature of the aircraft was that it was built out of fibreglass-reinforced paper – it was intended that the aircraft "kit" would be marketed printed on paper. The builder would cut out the parts and laminate them between fibreglass mats to build up the structure of the aircraft.

The Micro-IMP was ultimately a disappointment because its powerplant (taken from the Citroën 2CV) proved unsuitable, and a projected higher-powered version of the engine did not eventually become available. Holcomb later built a refined version with a different powerplant as the Ultra-IMP.

Specifications (Micro-IMP, Citroen engine, performance estimated)

Data from Jane's All The World's Aircraft 1982–83^[1]

General characteristics

Crew: 1
Length: 15 ft 0 in (4.57 m)
Wingspan: 27 ft 0 in (8.23 m)
Height: 4 ft 0 in (1.22 m)
Aspect ratio: 9:1
Airfoil: NASA GA(PC)-1
Empty weight: 260 lb (118 kg)
Max takeoff weight: 525 lb (238 kg)
Fuel capacity: 7 US Gallons (26.5 L)
Powerplant: 1 × Citroën air-cooled flat-twin piston engine, 25 hp (19 kW)

Performance

Maximum speed: 120 mph (190 km/h, 100 kn)
Cruise speed: 100 mph (160 km/h, 87 kn) (econ cruise)
Stall speed: 48 mph (77 km/h, 42 kn)
Service ceiling: 10,000 ft (3,000 m)
Rate of climb: 500 ft/min (2.5 m/s)

References

^ Taylor 1982, pp. 524–525.

John W. R. Taylor. Jane's All The World's Aircraft 1982–83. London:Jane's Yearbooks, 1982. ISBN 0-7106-0748-2.

[Janes_82_p524-5-1] Taylor 1982, pp. 524–525.

[1]

Specifications (Micro-IMP, Citroen engine, performance estimated)

See also

References