Rand Robinson KR-2S
9,609 FX6Aviaton
1.9 years ago
WIKIPEDIA:
The Rand Robinson KR-1 is a single-seat, single-engine sport aircraft designed in the United States in the early 1970s and marketed for homebuilding. A two-seat version is marketed as the KR-2. It is a low-wing cantilever monoplane of conventional design with an enclosed cockpit and tailwheel undercarriage. As originally designed, the main undercarriage units of the KR-1 and basic KR-2 were manually retractable, folding backwards into the wings, while the KR-2T tandem-seat version had fixed tricycle undercarriage. However, some builders choose fixed tailwheel or even fixed tricycle undercarriage for KR-1s and KR-2s.
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Specifications
General Characteristics
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- Wingspan 42.6ft (13.0m)
- Length 29.4ft (9.0m)
- Height 10.4ft (3.2m)
- Empty Weight 3,820lbs (1,732kg)
- Loaded Weight 7,971lbs (3,615kg)
Performance
- Horse Power/Weight Ratio 0.125
- Wing Loading 27.9lbs/ft2 (136.1kg/m2)
- Wing Area 285.9ft2 (26.6m2)
- Drag Points 3079
Parts
- Number of Parts 71
- Control Surfaces 7
- Performance Cost 297