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[edit]
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)[edit]
Data from Flight International
General characteristics
- Crew: 1
- Capacity: 1 passenger
- Powerplant: 1 × Volkswagen air-cooled engine horizontally opposed piston
Performance
See also[edit]
Related development
Aircraft of comparable role, configuration, and era
References[edit]
- ^ Sport Aviation: 49. March 1975.
{{cite journal}}: Missing or empty|title=(help) - ^ Flight International. 22 August 1977.
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