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The Kh-28 (Russian: Х-28; Nisan-28; NATO: AS-9 'Kyle') was the first Soviet anti-radiation missile (ARM) for tactical aircraft. It entered production in 1973 and is still carried on some Sukhoi Su-22s in developing countries but is no longer in Russian service. Use of the Kh-28 was restricted by its weight, limited seeker head, bulk and fuelling…
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missile soviet system seeker russian service isbn could aircraft use design su-17m 1973 operational iraq air one first arm similar
| Subject | Predicate | Object | Confidence | Src |
|---|---|---|---|---|
| Kh-28 | .mw-parser-output .tooltip-dotted{border-bottom:1px dotted;cursor:help}Maximum speed | Mach 3.0 | 1.00 | infobox |
| Kh-28 | Designer | Alexander Yakovlevich Bereznyak | 1.00 | infobox |
| Kh-28 | Diameter | 43 cm (16.9 in) | 1.00 | infobox |
| Kh-28 | Engine | Two-stage liquid-fuel rocket | 1.00 | infobox |
| Kh-28 | Guidance system | Inertial guidance with passive radar seeker | 1.00 | infobox |
| Kh-28 | In service | 1973–current | 1.00 | infobox |
| Kh-28 | Launch platform | Su-17M/Su-20/Su-22M, Su-24M, Tu-16, MiG-25BM, MiG-27, Tu-22M | 1.00 | infobox |
| Kh-28 | Length | 597 cm (19 ft 7 in) | 1.00 | infobox |
| Kh-28 | Manufacturer | MKB Raduga | 1.00 | infobox |
| Kh-28 | Mass | 720 kg (1,590 lb) | 1.00 | infobox |
| Kh-28 | Operational range | 110 km (59 nmi) | 1.00 | infobox |
| Kh-28 | Place of origin | Soviet Union | 1.00 | infobox |
| Kh-28 | Type | air-launched anti-radiation missile | 1.00 | infobox |
| Kh-28 | Used by | FSU, Warsaw Pact, India, Iraq, Vietnam | 1.00 | infobox |
| Kh-28 | Warhead | Blast fragmentation | 1.00 | infobox |
| Kh-28 | Warhead weight | 160 kg (353 lb) | 1.00 | infobox |
| Kh-28 | Wingspan | 193 cm (6 ft 4.0 in) | 1.00 | infobox |
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