SJJ-2 Tariq: Difference between revisions
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==History== | |||
==Design== | |||
==Variants== | |||
==Performance== |
Latest revision as of 14:04, 19 April 2020
SJJ-2 Tariq | |
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Type | Short-range air-to-air missile |
Place of origin | Riysa |
Service history | |
In service | 1963-1990 (Riysian Arab Air Force) |
Production history | |
Designer | Antara Special Research Office |
Unit cost | $94,000 (SJJ-2-360, refurbished) |
Produced | 1962-1989 (Riysa) |
Specifications | |
Weight | 90.6 kg |
Length | 2.75 m |
Diameter | 155 mm |
Warhead | 12.5 kg continuous-rod |
Detonation mechanism | Contact, laser proximity |
Engine | Solid-fuel rocket |
Operational range | 38 km |
Speed | Mach 3 |
Guidance system | Infrared |
Launch platform | Aircraft |