KD-88: Difference between revisions
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| wingspan = |
| wingspan = |
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| speed = [[Mach (speed)|Mach]] 0.85 |
| speed = [[Mach (speed)|Mach]] 0.85 |
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| vehicle_range = 200 km <ref>{{Cite web|url=https://www.globalsecurity.org/military/world/china/kd-88.htm|title=KD-88 air-to-surface missile|website=www.globalsecurity.org}}</ref> |
| vehicle_range = 200 km <ref>{{Cite web|url=https://www.globalsecurity.org/military/world/china/kd-88.htm|title=KD-88 air-to-surface missile|website=www.globalsecurity.org}}</ref><br>300 km (AKF-088C)<ref>https://chinese-military-aviation.blogspot.com/p/missiles-ii.html</ref> |
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| ceiling = |
| ceiling = |
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| altitude = |
| altitude = |
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| filling = |
| filling = 320 kg warhead |
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| guidance = [[Charge-coupled device|CCD/TV-seeker]]<ref name="harpia"/> for KD-88 or [[Thermography|imaging infrared (IIR)]]<ref name="harpia"/> for KD-88A |
| guidance = [[Charge-coupled device|CCD/TV-seeker]]<ref name="harpia"/> for KD-88 or [[Thermography|imaging infrared (IIR)]]<ref name="harpia"/> for KD-88A |
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| detonation = |
| detonation = |
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[[File:YJ-83J Missile 20170902.jpg|thumb|right|YJ-83J]] |
[[File:YJ-83J Missile 20170902.jpg|thumb|right|YJ-83J]] |
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'''KD-88''' (Kongdi-88) is a [[Standoff missile|standoff land attack missile]] built by [[China Aerospace Science and Technology Corporation]] (CASC). Its export version is called '''TL-17'''. It can be launched from a fighter aircraft or a bomber. It features a turbojet engine with cruising speeds of Mach 0.8 to Mach 0.85, and a range of {{convert|200|km|mi}}. Although comparable in size, configuration and capabilities, the KD-88 is not a true member of YJ-8 family.<ref name="harpia"/> |
'''KD-88''' (Kongdi-88) is a [[Standoff missile|standoff land attack missile]] built by [[China Aerospace Science and Technology Corporation]] (CASC). Its export version is called '''TL-17'''. It can be launched from a fighter aircraft or a bomber. It features a turbojet engine with cruising speeds of Mach 0.8 to Mach 0.85, and a range of {{convert|200|km|mi}}. Although comparable in size, configuration and capabilities, the KD-88 is not a true member of YJ-8 family.<ref name="harpia"/> |
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==Variants== |
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*'''KD-88''' |
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*'''KD-88A''' |
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*'''KD-88B''' |
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*'''AKF-088C''' |
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*'''TL-17''' |
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*'''TL-7A/B/C''' |
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==Operators== |
==Operators== |
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Revision as of 06:08, 28 April 2024
| KD-88 | |
|---|---|
| Type | Medium-range air-to-surface missile |
| Place of origin | China |
| Service history | |
| In service | 2006[1] |
| Used by | China |
| Production history | |
| Designer | China Aerospace Science and Technology Corporation |
| Manufacturer | Hongdu Aviation Industry Corporation |
| Specifications | |
| Mass | 0.6 ton |
| Length | 4.7 meter |
| Diameter | 0.3602 meter |
| Warhead | 320 kg warhead |
| Engine | turbojet |
| Propellant | liquid fuel |
Operational range | 200 km [2] 300 km (AKF-088C)[3] |
| Maximum speed | Mach 0.85 |
Guidance system | CCD/TV-seeker[1] for KD-88 or imaging infrared (IIR)[1] for KD-88A |
Launch platform | JH-7A J-10C J-16 J-15 |
KD-88 (Kongdi-88) is a standoff land attack missile built by China Aerospace Science and Technology Corporation (CASC). Its export version is called TL-17. It can be launched from a fighter aircraft or a bomber. It features a turbojet engine with cruising speeds of Mach 0.8 to Mach 0.85, and a range of 200 kilometres (120 mi). Although comparable in size, configuration and capabilities, the KD-88 is not a true member of YJ-8 family.[1]
Variants
- KD-88
- KD-88A
- KD-88B
- AKF-088C
- TL-17
- TL-7A/B/C
Operators
References
- ^ a b c d Rupprecht, Andreas (29 October 2018). Modern Chinese Warplanes - Chinese Air Force. Harpia Publishing. p. 116. ISBN 978-0-9973092-6-3.
- ^ "KD-88 air-to-surface missile". www.globalsecurity.org.
- ^ https://chinese-military-aviation.blogspot.com/p/missiles-ii.html
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