| KD-88 / KD-88A | |
|---|---|
KD-88A is the imaging infrared guided version of the KD-88 | |
| Type | Medium-range air-to-surface missile |
| Place of origin | China |
| Service history | |
| In service | 2006 |
| Used by | China |
| Production history | |
| Manufacturer | Hongdu Aviation Industry Corporation |
| Specifications | |
| Mass | 600 kg (1,300 lb) |
| Length | 470 cm (15.4 ft) |
| Diameter | 36.02 cm (14.18 in) |
| Warhead | 165 kg (364 lb) warhead |
| Engine | turbojet |
| Propellant | liquid fuel |
Operational range | 200 km (120 mi; 110 nmi) |
| Maximum speed | Mach 0.85 |
Guidance system | CCD/TV-seeker for KD-88 or imaging infrared (IIR) for KD-88A |
Launch platform | JH-7A J-10C J-16 J-15 |
The KD-88 (Kongdi-88; Chinese: 空地-88) is a standoff land attack missile built by Hongdu Aviation Industry Corporation and exported by China National Aero-Technology Import & Export Corporation (CATIC). Its export version is called TL-7 and TL-17.
KD-88 is derived from YJ-83 missile. KD-88 uses the body of YJ-83 but replaces the seeker with CCD/TV-seeker. The export version is called TL-7 (Chinese: 天龙-7; lit. 'Sky Dragon-7'). The KD-88A variant uses an imaging infrared (IIR) seeker for terminal inferred homing. TL-17 is the IIR variant made for export.
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 the YJ-8 family.
The KD-88 can be found on the Shenyang J-11 and Shenyang J-15 multi-role aircraft.
The KD-88 is designated AKD-88 (K/AKD88) in the PLAAF service.
