Rand-Robinson KR-3
KR-3 | |
---|---|
Role | Homebuilt aircraft |
National origin | United States |
Designer | Ken Rand |
Introduction | 1977 |
|
The Rand-Robinson KR-3 is an American amphibious aircraft that was designed by Ken Rand.[1]
Design and development
The KR-3 is a two-seat composite construction amphibious aircraft. The landing gear is hydraulically retractable. The prototype was demonstrated at the EAA airshow in 1977, demonstrating water taxi tests.[2]
Specifications (KR-3)
Data from Flight International
General characteristics
- Crew: 1
- Capacity: 1 passenger
- Powerplant: 1 × Volkswagen air-cooled engine horizontally opposed piston
Performance
See also
- Related development
- Aircraft of comparable role, configuration and era
References
This article is issued from Wikipedia - version of the 11/6/2015. The text is available under the Creative Commons Attribution/Share Alike but additional terms may apply for the media files.