LIPNUR Belalang: Perbedaan antara revisi
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{{Infobox Aircraft |
{{Infobox Aircraft |
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|name= Belalang |
|name= Belalang |
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|image= |
|image= |
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|caption=Belalang |
|caption=Belalang |
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|type= |
|type= Pesawat ringan |
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|manufacturer=LIPNUR |
|manufacturer=LIPNUR |
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|designer= |
|designer= Nurtanio |
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|first flight= |
|first flight= |
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|introduced= |
|introduced= |
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|number built= |
|number built= |
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|unit cost= |
|unit cost= |
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|developed from= |
|developed from= Piper J-3 Cub |
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|variants with their own articles= |
|variants with their own articles= |
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}} |
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'''Belalang ''' adalah pesawat produksi [[LIPNUR]] cikal bakal dari [[PT Dirgantara Indonesia]] |
'''Belalang ''' adalah pesawat produksi [[LIPNUR]] cikal bakal dari [[PT Dirgantara Indonesia]]. Pesawat ini merupakan versi sayap rendah dari [[Piper J-3 Cub]] yang saat itu sudah dimiliki Indonesia. Purwarupa Nu-85 terbang pertama kali pada 17 April 1958 dan produksi pertama Nu-90 dilakukan pada 1959. Pesawat ini digunakan sebagai pesawat latih di [[TNI AU]].<ref>http://www.flightglobal.com/pdfarchive/view/1962/1962%20-%201288.html</ref> |
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== Varian == |
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* '''Belalang 85''' - purwarupa |
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* '''Belalang 90''' - pesawat produksi, diproduksi 5 buah |
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* '''Belalang 90A''' - Mesin Continental O-200 75 kW (100 hp) menggantikan [[Continental C-90]]-12F 67 kW (90 hp) yang digunakan sebelumnya, kanopi geser, bagian roda yang diubah.<ref name="Janes 65 p83">Taylor 1965, p.83.</ref> |
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== Spesifikasi (90A) == |
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{{aircraft specifications |
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|jet or prop?=prop<!-- options: jet/prop/both/neither --> |
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|ref=Jane's All The World's Aircraft 1965-66 <ref name="Janes 65 p83"/> |
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General characteristics |
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|crew=2 |
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|capacity= |
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|payload main= |
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|payload alt= |
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|length main= 7.70 m |
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|length alt=25 ft 3½ in |
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|span main=9.50 m |
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|span alt=31 ft 1 in |
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|height main=2.03 m |
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|height alt=6 ft 8 in |
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|area main= 15.0 m² |
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|area alt= 161.5 sq ft |
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|airfoil=USA-35B |
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|aspect ratio=6 |
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|empty weight main= 230 kg |
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|empty weight alt= 506 lb |
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|loaded weight main= |
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|loaded weight alt= |
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|useful load main= |
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|useful load alt= |
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|max takeoff weight main= 330 kg |
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|max takeoff weight alt= 726 lb |
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|more general= |
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Powerplant |
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|engine (prop)=[[Continental O-200]]-A |
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|type of prop=air-cooled [[flat-four]] |
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|number of props=1 |
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|power main= 75 kW |
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|power alt=100 hp |
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|power original= |
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|propeller or rotor?=<!-- options: propeller/rotor --> |
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|propellers= |
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|number of propellers per engine= |
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Performance |
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|max speed main= |
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|max speed alt= |
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|max speed more= |
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|cruise speed main= 130 km/h |
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|cruise speed alt=70 knots, 80 mph |
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|cruise speed more= |
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|stall speed main= |
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|stall speed alt= |
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|stall speed more= |
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|never exceed speed main= |
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|never exceed speed alt= |
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|range main= 564 km |
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|range alt=304 [[nautical mile|nmi]], 350 miles<ref name="Flight 61 p136">[http://www.flightglobal.com/pdfarchive/view/1962/1962%20-%201288.html "Asia's Aircraft Industries:NU-90 Belalang"]. ''[[Flight International]]'', 26 July 1962. p. 136.</ref> |
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|range more= |
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|combat radius main= |
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|ferry range main= |
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|ferry range alt= |
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|ferry range more= |
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|endurance= |
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|ceiling main=3,700 m |
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|ceiling alt= 12,000 ft<ref name="Flight 61 p136"/> |
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|ceiling more= |
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|climb rate main= 2.3 m/s |
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|climb rate alt= 460 ft/min |
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|climb rate more= |
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|sink rate main= |
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|sink rate alt= |
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|sink rate more= |
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|loading main= |
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|loading alt= |
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|thrust/weight= |
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|power/mass main= |
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|power/mass alt= |
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|more performance= |
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Armament |
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|armament=<!-- if you want to use the following specific parameters, do not use this line at all--> |
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|guns= |
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|bombs= |
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|rockets= |
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|missiles= |
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|hardpoints= |
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|hardpoint capacity= |
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|avionics= |
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}} |
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== Lihat juga == |
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* [[LIPNUR Kunang]] |
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== Referensi == |
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{{reflist}} |
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* [[John W. R. Taylor|Taylor, John W. R.]] ''Jane's All The World's Aircraft 1965-66''. London: Sampson Low, Marston, 1965. |
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{{Pesawat Dirgantara Indonesia}} |
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{{perusahaan-stub}} |
{{perusahaan-stub}} |
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[[Kategori:Indonesian military trainer aircraft 1950–1959]] |
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[[Kategori:Pesawat terbang Nusantara]] |
[[Kategori:Pesawat terbang Nusantara]] |
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[[en:LIPNUR Belalang]] |
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[[fi:LIPNUR Belalang]] |
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Revisi per 1 November 2022 09.16
| Tipe | Pesawat ringan |
|---|---|
| Perancang | Nurtanio |
| Pengguna utama | Indonesia |
| Acuan dasar | Piper J-3 Cub |
Belalang adalah pesawat produksi LIPNUR cikal bakal dari PT Dirgantara Indonesia. Pesawat ini merupakan versi sayap rendah dari Piper J-3 Cub yang saat itu sudah dimiliki Indonesia. Purwarupa Nu-85 terbang pertama kali pada 17 April 1958 dan produksi pertama Nu-90 dilakukan pada 1959. Pesawat ini digunakan sebagai pesawat latih di TNI AU.[1]
Varian
- Belalang 85 - purwarupa
- Belalang 90 - pesawat produksi, diproduksi 5 buah
- Belalang 90A - Mesin Continental O-200 75 kW (100 hp) menggantikan Continental C-90-12F 67 kW (90 hp) yang digunakan sebelumnya, kanopi geser, bagian roda yang diubah.[2]
Spesifikasi (90A)
Data dari Jane's All The World's Aircraft 1965-66 [2]
Ciri-ciri umum
- Kru: 2
- Panjang: 7.70 m
- Rentang sayap: 9.50 m
- Tinggi: 2.03 m
- Luas sayap: 15.0 m²
- Airfoil: USA-35B
- Aspect ratio: 6
- Berat kosong: 230 kg
- Berat maksimum saat lepas landas: 330 kg
- Mesin: 1 × Continental O-200-A air-cooled flat-four, 75 kW (100 hp)
Kinerja
- Laju jelajah: 130 km/h (70 knots, 80 mph)
- Jangkauan: 564 km
- Langit-langit batas: 3,700 m
- Laju tanjak: 2.3 m/s
Lihat juga
Referensi
- ^ http://www.flightglobal.com/pdfarchive/view/1962/1962%20-%201288.html
- ^ a b Taylor 1965, p.83.
- ^ a b "Asia's Aircraft Industries:NU-90 Belalang". Flight International, 26 July 1962. p. 136.
- Taylor, John W. R. Jane's All The World's Aircraft 1965-66. London: Sampson Low, Marston, 1965.
 | Artikel bertopik perusahaan ini adalah sebuah rintisan. Anda dapat membantu Wikipedia dengan mengembangkannya. |