Kh-59 ovod
From Wikipedia, the free encyclopedia
Kh-59 ovod (gô-gú: Х-59 овод 'gadfly' (bîng [en]); AS-13 'kingbolt' (tio̍k)) sī Gôlôsu tēn-sī tsè-tō [en] sûn-i̍k tō-tān [en], kū-iú nn̄g-kip kóo-thé jên-liāu thui-tsìn hē-thóng, siā-tîng 200 km. Kh-59M ovod-m (AS-18 'kazoo') sī tsi̍t-tsióng kū-iú koh-khah tuā ê tān-tiôu [en] hām "o-lûn phùn-siā [en]" (turbojet) e̋̋n-z̦ín ê ên-sin-hîng. Kh-59 ovod tsú-iàu sī tsi̍t-tsióng kàm tuì tē tō-tān [en], m̄-koh Kh-59MK ên-sin-hîng ê bo̍k-piau sī tsûn-kàm.[4]
Quick Facts Luī-hîng, Guân-sán-tē ...
Kh-59 ovod (NATO tāi-hō: AS-13 'kingbolt') Kh-59M ovod-m (AS-18 'kazoo') | |
---|---|
Kh-59MK teh 2009 MAKS hâng-tén [en] | |
Luī-hîng |
Cruise missile Air-launched cruise missile Air-to-surface missile Anti-ship missile Land-attack missile |
Guân-sán-tē | Soviet Union/Russia |
Ho̍k-i̍k kì-lo̍k | |
Ho̍k-i̍k kî-kan | 1980–bo̍ktsên |
Sú-iōng tsiá | Russia, China, India, Algeria |
Tsèn-tsing |
First Chechen War Second Chechen War Russo-Ukrainian War |
Sing-sán li̍k-sú | |
Set-kè-tsiá | MKB Raduga |
Sing-sán-siong | Tactical Missiles Corporation |
Ki-pún tsu-guân | |
Tāng-liōng | 930 kg (2,050 lb)[1] |
Tn̂g-tōo | 570 cm (220 in)[1] |
Ti̍t-kìng | 38.0 cm (15.0 in)[1] |
Tuâñ-thâu | Cluster or shaped-charge fragmentation[1] |
Warhead weight | 320 kg (705 lb)[2] |
| |
E̋n-z̩ín |
Kh-59: two-stage rocket Kh-59ME: rocket then R95TP-300[3] turbojet/turbofan |
I̍k-tén | 130 cm (51.2 in)[1] |
Ūn-tsok huān-uî |
Kh-59ME (export): 115 km (62 nmi)[1] Kh-59ME: 200 km (110 nmi) Kh-59MK: 285 km (150 nmi) Kh-59MK2: 290 km (160 nmi) |
Siōng-kuân sok-tōo | Mach 0.72–Mach 0.88 (548.07–669.86 mph; 882.03–1,078.04 km/h)[1] |
Tō-ín hē-thóng | Inertial guidance (then TV guidance), millimeter wave active radar seeker (Kh-59MK, Kh-59MK2 land attack version)[4] |
Huat-siā pêñ-tâi |
Kh-59ME: Su-30MK[1] Kh-59: Su-24M, MiG-27, Su-17M3/22M4, HAL Tejas, Su-30 MKI Su-25 and Su-30[5] Kh-59MK2: Su-57[6] |
Close