Hongdu JL-8: Perbedaan antara revisi
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== Desain ==
* '''Mesin:''' K-8 digerakan oleh [[Honeywell TFE731]]-2A-2A mesin [[turbofan]] modular dengan [[DEEC]] & [[sistem kontrol bahan bakar]] hidro-mekanis. Karena sanksi USA atas Tiongkok , versi selanjutnya digerakan oleh AL-25 dan WS-11 (Tiongkok).
* '''Layout Kokpit:'''disain untuk memenuhi standar Spesifikasi Militer terbaru. [[EFIS]] buatan [[Collins]] dipasang di kokpit depan dan belakang. [[Ultra high frequency|UHF]]/[[VHF]] communication system, [[TACAN]]/[[RADIO COMPASS]] & [[ILS]] juga tersedia tergantung kebutuhan konsumen.
* '''Sistem Penyelamatan: ''' 2 [[kursi lontar]][[Martin Baker MK-10L]] otomatis penuh berpendorong roket [[zero-zero]] (dalam kecepatan 0 km/j dan ketinggian 0m mampu beroperasi).
* '''[[Environmental control system]] (ECS):''' [[Allied Signal]] ECS dengan kemampuan [[AC]]( [[air conditioning]] ) bahakan didarat pada [[suhu ambient]] -40
* '''Sistem bahan bakar:''' Muatan total BBM pada 2 tangki karet pada badan pesawat dan sebuah tangki didalam sayap adalah 1720 lb. Kapasitas tiap [[drop tank]] adalah 250 L.
* '''Sistem kontrol penerbangan:''' [[Permukaan Kontrol Penerbangan]] Konvensional yang dikontrol oleh sistem transmisi rigid push-rod dan dioperasikan secara elektris maupun hidrolis.
== Operator ==
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== Data Teknis ==
=== data utama ===
* '''Rated power:''' 3600 lbf max [[static thrust]] at sea level
* '''SFC:''' 0.502 lb/lbf.h (Max static thrust)
* '''Air flow:''' 115 lb/s (take-off and max continuous)
* '''Engine net weight:''' 812 lb
* '''Pressure ratio:''' 13.9
* '''Bypass ratio"''' 2.67
=== Dimensi ===
* '''Panjang:''' 11.6 m
* '''Tinggi:''' 4.21 m
* '''Luas sayap:''' 17.02 m²
* '''Rentang sayap:''' 9.63 m
* '''Wheel track:''' 2.54 m
* '''Wheel base:''' 4.442 m
=== Berat ===
* '''Normal take-off weight:''' 3700 kg
* '''Useful load:''' 943 kg
* '''Internal fuel capacity:''' 780 kg
* '''Empty weight:''' 2757 kg
* '''Max take-off weight:''' 4332 kg
=== Performa terbang ===
* '''Max level speed:''' 800 km/h
* '''Rate of climb at sea level:''' 30 m/s
* '''Service ceiling:''' 13,600 m
* '''Built-in range:''' 1560 km
* '''Ferry range (with drop tanks):''' 2140 km
* '''Endurance:''' 3.2 hrs
* '''Max endurance (with drop tanks):''' 4.2 h
* '''Unstick speed:''' 185 km/h
* '''Touchdown speed:''' 160 km/h
* '''Take-off ground run:''' 440 m
* '''Landing ground run:''' 530 m
* '''Limit load factor:''' +7.33/-3.0 ''g''
== Literatur ==
* Donald, David and Lake, Jon, ed. ''The Encyclopedia of World Military Aircraft'' (2000) p.391-392. NY: Barnes & Noble. ISBN 0-7607-2208-0
== Pesawat sejenis ==
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== Pranala luar ==
* [http://www.fas.org/man/dod-101/sys/ac/row/k-8.htm K-8 Karakorum at FAS.org]
* [http://www.aerospaceweb.org/aircraft/attack/k8/ K-8 Karakorum at Aerospaceweb.org]
* [http://www.sinodefence.com/airforce/trainer/jl8.asp JL-8 at Chinese Defence Today]
* [http://www.pakistanidefence.com/DefenceProduction/PAC/K8_Manufacturing.htm Karakorum-8 at PakistaniDefence.com]
* [http://www.pakdef.info/pakmilitary/airforce/ac/k8.html K-8 Karakorum at PakDef.info]
* [http://www.china-defense-mashup.com/?page_id=5298 China PLA Air Force Power]
* [http://cnair.top81.cn/F-7_J-7_J-8.htm J-8D Finback]
{{Chinese Military Aircraft}}
[[Kategori:Pesawat latih militer]]
[[Kategori:Pesawat jet]]
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