Kh-35
| Tempat asal | Soviet Union |
|---|---|
| Dihasilkan | 1996 for export, 2003 for Russia |
| Sistempemanduan | inertial guidance and ARGS-35E X-band terminal active radar homing[4] |
| Dalam perkhidmatan | 2003 |
| Kelajuan | Mach 0.8–Mach 0.95 (609–723 mph; 980–1,164 km/h) |
| Direka | 1983-2003 |
| Warhead weight | 145 kg (320 lb)[2] |
| Lebar sayap | 133 cm (52.4 in)[2] |
| Warhead | HE fragmentation shaped charge |
| Berat | 520 kg (1,150 lb)[2] 610 kg (1,340 lb)[2] (heli version) |
| Panjang | 385 cm (152 in)[2] 440 cm (173 in)[2] (heli version) |
| Pereka | Zvezda |
| Altitud penerbangan | 10-15 m en route and about 4 m at terminal area |
| Enjin | R95-300 Turbojet Kh-35 / Turbofan Kh-35U 360 kgf |
| Kos unit | $500,000 (2010)[1] |
| Digunakan oleh | Tentera laut Russia Tentera laut India Tentera laut Vietnam |
| Jarakoperasi | 130 km (70 nmi) 300 km (160 nmi) (2015)[3] |
| Pengeluar | Tactical Missiles Corporation |
| Platformpelancaran | Tupolev Tu-142, Su-24, MiG-29M/K, Sukhoi Su-35, Su-27SM, Su-30MKI//SM, Su-34, HAL Tejas, Ka-27, Ka-28,[2][5] Ka-52, T-50,[6] also ships and boats, coastal, LACM, TEL variants. |
| Diameter | 42.0 cm (16.5 in)[2] |
| Jenis | peluru berpandu udara ke permukaan peluru berpandu permukaan ke permukaan peluru berpandu krus peluru berpandu anti-kapal |
| Bebaling | kerosene |
