LIPNUR Belalang: Perbedaan antara revisi
Konten dihapus Konten ditambahkan
k kat |
NikolasKHF (bicara | kontrib) Fitur saranan suntingan: 2 pranala ditambahkan. |
||
| (20 revisi perantara oleh 16 pengguna tidak ditampilkan) | |||
| Baris 1: | Baris 1: | ||
{{Infobox Aircraft |
{{Infobox Aircraft |
||
|name= Belalang |
|name= Belalang |
||
|image= |
|image= |
||
|caption=Belalang |
|caption=Belalang |
||
|type= |
|type= Pesawat ringan |
||
|manufacturer=LIPNUR |
|manufacturer=LIPNUR |
||
|designer= |
|designer= Nurtanio |
||
|first flight= |
|first flight= |
||
|introduced= |
|introduced= |
||
| Baris 11: | Baris 11: | ||
|status= |
|status= |
||
|primary user=Indonesia |
|primary user=Indonesia |
||
|more users=<!--up to three more. please separate with |
|more users=<!--up to three more. please separate with {{br}}.--> |
||
|produced= |
|produced= |
||
|number built= |
|number built= |
||
|unit cost= |
|unit cost= |
||
|developed from= |
|developed from= Piper J-3 Cub |
||
|variants with their own articles= |
|variants with their own articles= |
||
}} |
}} |
||
'''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> |
||
== Varian == |
|||
{{rintisan}} |
|||
* '''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.<ref name="Janes 65 p83">Taylor 1965, p.83.</ref> |
|||
== Spesifikasi (90A) == |
|||
[[Kategori:Dirgantara Indonesia]] |
|||
{{aircraft specifications |
|||
<!-- if you do not understand how to use this template, please ask at [[Wikipedia talk:WikiProject Aircraft]] --> |
|||
|plane or copter?=plane<!-- options: plane/copter --> |
|||
|jet or prop?=prop<!-- options: jet/prop/both/neither --> |
|||
<!-- Now, fill out the specs. Please include units where appropriate (main comes first, alt in parentheses). If an item doesn't apply, like capacity, leave it blank. |
|||
--> |
|||
|ref=Jane's All The World's Aircraft 1965-66 <ref name="Janes 65 p83"/> |
|||
<!-- |
|||
General characteristics |
|||
--> |
|||
|crew=2 |
|||
|capacity= |
|||
|payload main= |
|||
|payload alt= |
|||
|length main= 7.70 m |
|||
|length alt=25 ft 3½ in |
|||
|span main=9.50 m |
|||
|span alt=31 ft 1 in |
|||
|height main=2.03 m |
|||
|height alt=6 ft 8 in |
|||
|area main= 15.0 m² |
|||
|area alt= 161.5 sq ft |
|||
|airfoil=USA-35B |
|||
|aspect ratio=6 |
|||
|empty weight main= 230 kg |
|||
|empty weight alt= 506 lb |
|||
|loaded weight main= |
|||
|loaded weight alt= |
|||
|useful load main= |
|||
|useful load alt= |
|||
|max takeoff weight main= 330 kg |
|||
|max takeoff weight alt= 726 lb |
|||
|more general= |
|||
<!-- |
|||
Powerplant |
|||
--> |
|||
|engine (prop)=[[Continental O-200]]-A |
|||
|type of prop=air-cooled [[flat-four]] |
|||
|number of props=1 |
|||
|power main= 75 kW |
|||
|power alt=100 hp |
|||
|power original= |
|||
|propeller or rotor?=<!-- options: propeller/rotor --> |
|||
|propellers= |
|||
|number of propellers per engine= |
|||
|propeller diameter main= |
|||
|propeller diameter alt= |
|||
<!-- |
|||
Performance |
|||
--> |
|||
|max speed main= |
|||
|max speed alt= |
|||
|max speed more= |
|||
|cruise speed main= 130 km/h |
|||
|cruise speed alt=70 knots, 80 mph |
|||
|cruise speed more= |
|||
|stall speed main= |
|||
|stall speed alt= |
|||
|stall speed more= |
|||
|never exceed speed main= |
|||
|never exceed speed alt= |
|||
|range main= 564 km |
|||
|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> |
|||
|range more= |
|||
|combat radius main= |
|||
|combat radius alt= |
|||
|combat radius more= |
|||
|ferry range main= |
|||
|ferry range alt= |
|||
|ferry range more= |
|||
|endurance= |
|||
|ceiling main=3,700 m |
|||
|ceiling alt= 12,000 ft<ref name="Flight 61 p136"/> |
|||
|ceiling more= |
|||
|climb rate main= 2.3 m/s |
|||
|climb rate alt= 460 ft/min |
|||
|climb rate more= |
|||
|sink rate main= |
|||
|sink rate alt= |
|||
|sink rate more= |
|||
|loading main= |
|||
|loading alt= |
|||
|thrust/weight= |
|||
|power/mass main= |
|||
|power/mass alt= |
|||
|more performance= |
|||
<!-- |
|||
Armament |
|||
--> |
|||
|armament=<!-- if you want to use the following specific parameters, do not use this line at all--> |
|||
|guns= |
|||
|bombs= |
|||
|rockets= |
|||
|missiles= |
|||
|hardpoints= |
|||
|hardpoint capacity= |
|||
|avionics= |
|||
}} |
|||
== Lihat juga == |
|||
* [[LIPNUR Kunang]] |
|||
== Referensi == |
|||
{{reflist}} |
|||
* [[John W. R. Taylor|Taylor, John W. R.]] ''Jane's All The World's Aircraft 1965-66''. London: Sampson Low, Marston, 1965. |
|||
{{Pesawat Dirgantara Indonesia}} |
|||
{{perusahaan-stub}} |
|||
[[Kategori:Indonesian military trainer aircraft 1950–1959]] |
|||
[[Kategori:Pesawat terbang Nusantara]] |
|||
Revisi terkini sejak 22 Oktober 2024 01.17
| 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
[sunting | sunting sumber]- 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)
[sunting | sunting sumber]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
[sunting | sunting sumber]Referensi
[sunting | sunting sumber]- ^ 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. |