Kh-28 (NATO reporting name: AS-9 'Kyle') | |
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Type | air-launched anti-radiation missile |
Place of origin | Soviet Union |
Service history | |
In service | 1973–current |
Used by | FSU,[1] Warsaw Pact,[1] India,[1] Iraq,[1] Vietnam[1] |
Production history | |
Designer | Alexander Yakovlevich Bereznyak |
Manufacturer | MKB Raduga |
Specifications | |
Mass | 720 kg (1,590 lb)[2] |
Length | 597 cm (19 ft 7 in)[2] |
Diameter | 43 cm (16.9 in)[2] |
Wingspan | 193 cm (6 ft 4.0 in)[2] |
Warhead | Blast fragmentation[1] |
Warhead weight | 160 kg (353 lb)[2] |
Engine | Two-stage liquid-fuel rocket[2] |
Operational range | 110 km (59 nmi) [3] |
Maximum speed | Mach 3.0[2] |
Guidance system | Inertial guidance with passive radar seeker[1] |
Launch platform | Su-17M/Su-20/Su-22M, Su-24M, Tu-16, MiG-25BM, MiG-27, Tu-22M[4] |
The Kh-28 (Russian: Х-28; Nisan-28; NATO: AS-9 'Kyle') was the first Soviet anti-radiation missile (ARM) for tactical aircraft.[1] It entered production in 1973 and is still carried on some Sukhoi Su-22s in developing countries but is no longer in Russian service.[1] Use of the Kh-28 was restricted by its weight, limited seeker head, bulk and fuelling requirements, and it was superseded by the smaller, solid-fuel Kh-58 (AS-11 'Kilter') in the early 1980s.
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