LIPNUR Kunang

The LIPNUR Kunang was a single-seat sports plane built in Indonesia that first flew in 1958 in the hope that it would inspire interest in aviation amongst Indonesian youth. The only example that was built was subsequently grounded. It was a single-seat monoplane of conventional layout with fixed tailwheel undercarriage.

Kunang
Role Sports aircraft
Manufacturer Angkatan Udara Republik Indonesia, Depot Penjelidikan, Pertjobaan dan Pembuatan/LIPNUR
First flight 1958

Specifications

Data from Jane's All The World's Aircraft 1961–62[1]

General characteristics

  • Crew: 1
  • Wingspan: 8.60 m (28 ft 3 in)
  • Height: 1.77 m (5 ft 10 in)
  • Wing area: 7.7 m2 (83 sq ft)
  • Aspect ratio: 9.6:1
  • Airfoil: NACA 2412
  • Empty weight: 160 kg (353 lb)
  • Gross weight: 260 kg (573 lb)
  • Fuel capacity: 15 l (4.0 US gal; 3.3 imp gal)
  • Powerplant: 1 × Volkswagen 4-cylinder air-cooled horizontally-opposed piston engine, 19 kW (25 hp)

Performance

  • Cruise speed: 137 km/h (85 mph, 74 kn)
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See also

References
  1. Taylor 1961, p. 95.
  • Taylor, John W. R. (1961). Jane's All The World's Aircraft 1961–62. London: Sampson Low, Marston & Company.
  • Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 62.
  • Harapan dan Tanggapan Pemerhati dan Mitra (in Indonesian)


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