ADI Condor
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The ADI Condor was a motor glider of unusual configuration built in the United States in 1981. While most motor gliders follow traditional sailplane layout, the Condor was of pod-and-boom configuration, with a pusher propeller at the rear of the central nacelle that seated the pilot and passenger in tandem. The single example of the aircraft was destroyed in a crash in late 1982 after an engine failure.
Of composite construction, the Condor was powered by a modified VW engine and had a wing area of 130 ft² (12 m²).
[edit] Specifications (ADI Condor)
This aircraft article is missing some (or all) of its specifications. If you have a source, you can help Wikipedia by adding them.General characteristics
- Crew: one pilot
- Capacity: one passenger
- Length: ()
- Wingspan: ()
- Height: ()
- Wing area: 130 ft² (12 m²)
- Powerplant: 1× modified VW engine, ()
Performance
[edit] See also
Related development
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