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LIPNUR Sikumbang

The LIPNUR Sikumbang (manufacturer designation X-01) was a low-wing monoplane of mixed construction built in Indonesia in 1954 as a COIN and anti-guerrilla-warfare aircraft. Of conventional configuration, it had fixed tricycle undercarriage and seated the pilot under a bubble canopy. A single example was built under the designation NU-200 in 1954, and another as the NU-225 in 1957. The latter machine was grounded in 1967.


Specifications (NU-200) edit

Data from Jane's All The World's Aircraft 1955–56[1]

General characteristics

  • Crew: 1
  • Length: 8.16 m (26 ft 9 in)
  • Wingspan: 10.61 m (34 ft 10 in)
  • Height: 3.35 m (11 ft 0 in)
  • Wing area: 16.9 m2 (182 sq ft)
  • Aspect ratio: 6.6:1
  • Airfoil: NACA 23015 at root, NACA 23009 at tip
  • Empty weight: 795 kg (1,753 lb)
  • Gross weight: 1,090 kg (2,403 lb)
  • Fuel capacity: 205 L (54 US gal; 45 imp gal)
  • Powerplant: 1 × de Havilland Gipsy Six air-cooled inverted six-cylinder inline engine, 150 kW (200 hp)
  • Propellers: 2-bladed fixed pitch

Performance

  • Maximum speed: 256 km/h (159 mph, 138 kn)
  • Cruise speed: 224 km/h (139 mph, 121 kn)
  • Range: 960 km (600 mi, 520 nmi)
  • Service ceiling: 5,030 m (16,500 ft)
  • Rate of climb: 5.1 m/s (1,000 ft/min)

See also edit

Aircraft of comparable role, configuration, and era

References edit

  1. ^ Bridgman 1955, p. 165.
  • Bridgman, Leonard (1955). Jane's All The World's Aircraft 1955–56. New York: The McGraw-Hill Book Company.
  • Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 61.



lipnur, sikumbang, manufacturer, designation, wing, monoplane, mixed, construction, built, indonesia, 1954, coin, anti, guerrilla, warfare, aircraft, conventional, configuration, fixed, tricycle, undercarriage, seated, pilot, under, bubble, canopy, single, exa. The LIPNUR Sikumbang manufacturer designation X 01 was a low wing monoplane of mixed construction built in Indonesia in 1954 as a COIN and anti guerrilla warfare aircraft Of conventional configuration it had fixed tricycle undercarriage and seated the pilot under a bubble canopy A single example was built under the designation NU 200 in 1954 and another as the NU 225 in 1957 The latter machine was grounded in 1967 NU 200 Sikumbang Role Counter insurgency aircraft Manufacturer Angkatan Udara Republik Indonesia Depot Penjelidikan Pertjobaan dan Pembuatan LIPNUR First flight 1954Specifications NU 200 editData from Jane s All The World s Aircraft 1955 56 1 General characteristicsCrew 1 Length 8 16 m 26 ft 9 in Wingspan 10 61 m 34 ft 10 in Height 3 35 m 11 ft 0 in Wing area 16 9 m2 182 sq ft Aspect ratio 6 6 1 Airfoil NACA 23015 at root NACA 23009 at tip Empty weight 795 kg 1 753 lb Gross weight 1 090 kg 2 403 lb Fuel capacity 205 L 54 US gal 45 imp gal Powerplant 1 de Havilland Gipsy Six air cooled inverted six cylinder inline engine 150 kW 200 hp Propellers 2 bladed fixed pitch Performance Maximum speed 256 km h 159 mph 138 kn Cruise speed 224 km h 139 mph 121 kn Range 960 km 600 mi 520 nmi Service ceiling 5 030 m 16 500 ft Rate of climb 5 1 m s 1 000 ft min See also editLIPNUR Belalang LIPNUR Kunang LIPNUR Super Kunang Aircraft of comparable role configuration and era Fletcher FD 25 American Electric Piranha SIAI Marchetti SF 260 Soko J 20 KragujReferences edit Bridgman 1955 p 165 Bridgman Leonard 1955 Jane s All The World s Aircraft 1955 56 New York The McGraw Hill Book Company Taylor Michael J H 1989 Jane s Encyclopedia of Aviation London Studio Editions p 61 Harapan dan Tanggapan Pemerhati dan Mitra nbsp This article on an aircraft of the 1950s is a stub You can help Wikipedia by expanding it vte Retrieved from https en wikipedia org w index php title LIPNUR Sikumbang amp oldid 1011492949, wikipedia, wiki, book, books, library,

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