Back Ch-55 Czech Ch-55 German Raduga Kh-55 Spanish خا-۵۵ Persian H-55 Finnish Kh-55 French H–55 Hungarian Kh-55 (keluarga peluru kendali) ID Kh-55 Italian Kh-55 (ミサイル) Japanese
 | This article needs additional citations for verification. (October 2015) |
 | It has been suggested that this article should be split into a new article titled Kh-101/102. (discuss) (October 2022) |
| Kh-55/65/101/102/555 AS-15 Kent | |
|---|---|
 Kh-55 in the Ukrainian Air Force Museum | |
| Type | Air-launched cruise missile |
| Place of origin | Soviet Union |
| Service history | |
| In service | 1983–present |
| Used by | Soviet Union, Russia, China, Iran |
| Wars | Syrian Civil War[1] 2022 Russian invasion of Ukraine[2] |
| Production history | |
| Designed | 1971–1981 |
| Manufacturer | Raduga OKB, KhAZ (Kharkiv), Novator (MZiK) & NPP Temp (Eka) NPO Strela (Oren), else |
| Produced | 1981 |
| Specifications | |
| Mass | 1,650 kg (3,640 lb) (Kh-65SE)[3] 2,400 kg (5,300 lb) (Kh-101)[4] |
| Length | 604 cm (19 ft 10 in) (Kh-65SE)[3] 745 cm (24 ft 5 in) (Kh-101)[4] |
| Diameter | 51.4 cm (20.2 in) (Kh-55/Kh-55SM) |
| Wingspan | 310 cm (122.0 in) (Kh-55/Kh-55SM) |
| Warhead | Thermonuclear weapon or Conventional warhead |
| Blast yield | 200kt Nuclear (Kh-55/Kh-55SM) |
| Engine | R95TP-300 Turbofan[5]/turbofan (Kh-55/Kh-55SM) 360-400 kgf (Kh-55/Kh-55SM) |
| Propellant | jet fuel |
Operational range | 2,500 km (1,300 nmi) (Kh-55) 3,000 km (1,600 nmi) (Kh-55SM) 600 km (320 nmi) (Kh-65SE)[3] 300 km, later 600 km (Kh-SD)[3] |
| Flight altitude | under 110 m/300 ft |
| Maximum speed | Mach 0.75 (KH-SD)[3] Mach 0.6-0.78 (Kh-101)[4] |
Guidance system | inertial guidance with Doppler radar/terrain map updates; Kh-SD had a TC/IIR terminal guidance system, and an alternative active radar homing seeker was proposed |
Launch platform | Tu-95MS, Tu-160, Su-34[6] |
The Kh-55 (Russian: Х-55[note 1], also known as RKV-500; NATO reporting name: AS-15 "Kent") is a Soviet/Russian subsonic air-launched cruise missile, designed by MKB Raduga in the 1970s. It has a range of up to 2,500 km (1,350 nmi) and can carry nuclear warheads. Kh-55 is launched exclusively from bomber aircraft and has spawned a number of conventionally armed variants mainly for tactical use, such as the Kh-65SE and Kh-SD, but only the Kh-101 and Kh-555 appear to have been put into service. The Kh-55 was not the basis of the submarine and ground-launched S-10 Granat or RK-55 Relief (SS-N-21 "Sampson" and SSC-X-4 "Slingshot") designed by NPO Novator. The RK-55 is very similar to the air-launched Kh-55 (AS-15 "Kent") but the Kh-55 has a drop-down turbofan engine and was designed by MKB Raduga.
- ^ "25 Russian long-range strategic bombers in action over Syria for the very first time". Theaviationist.com. 17 November 2015. Archived from the original on 20 November 2015. Retrieved 1 November 2017.
- ^ Douglas Barrie (1 April 2022). "Ukraine: Russia's air-launched cruise missiles coming up short". The International Institute for Strategic Studies. Archived from the original on 30 September 2022. Retrieved 15 September 2022.
- ^ a b c d e Cite error: The named reference
JSWSwas invoked but never defined (see the help page). - ^ a b c Cite error: The named reference
JDW-101was invoked but never defined (see the help page). - ^ "ОАО "АМНТК "Союз"". www.amntksoyuz.ru. Archived from the original on 5 December 2019. Retrieved 30 November 2019.
- ^ Cite error: The named reference
JSWS101was invoked but never defined (see the help page).
Cite error: There are <ref group=note> tags on this page, but the references will not show without a {{reflist|group=note}} template (see the help page).
© MMXXIII Rich X Search. We shall prevail. All rights reserved. Rich X Search