LIPNUR Belalang: Perbedaan antara revisi
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{{Infobox Aircraft
|name= Belalang
|image=
|caption=Belalang
|type= Pesawat ringan
|manufacturer=LIPNUR
|designer= Nurtanio
|first flight=
|introduced=
Baris 11:
|status=
|primary user=Indonesia
|more users=<!--up to three more. please separate with
|produced=
|number built=
|unit cost=
|developed from= Piper J-3 Cub
|variants with their own articles=
}}
'''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 ==
* '''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) ==
{{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]]
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