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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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General Characteristics

  • Created On Android
  • 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