R.530
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(Redirected from Matra R530)
Matra R.530 | |
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An R530 exhibited at the South African Air Force Museum, Swartkop
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Type | short-range air-to-air missile |
Service history | |
In service | 1962 [1] |
Production history | |
Manufacturer | Matra |
Specifications | |
Weight | 192 kg [1] |
Length | 3.28 m [1] |
Diameter | 263 mm [1] |
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Engine | two stage solid rocket,[1] Hotchkiss-Brandt/SNPE Antoinette rocket [2] 83.3 kN for 2.7 s + 6.5 s cruise[2] |
Wingspan | 1.1 m[2] |
Operational
range |
1.5 to 20 km [1] |
Speed | Mach 2.7 [1] |
Guidance
system |
Semi active radar homing and Infrared homing[3] |
Launch
platform |
Dassault Mirage F1 Dassault Mirage III [1] F-8 Crusader |
The Matra R.530 is a French medium to short range air-to-air missile. It was available in Infrared homing and SARH as the main armament of the Mirage III which was able to carry a single missile in the centerline, the Mirage F1, which carried 2 (1 of each type) under the wings, and the F-8 Crusader in the French Navy service.
Operators
Former operators
- Argentina
- Australia
- Brazil
- Cameroon
- Colombia
- France
- Egypt
- Iraq
- Israel
- Jordan
- Lebanon
- Morocco
- Pakistan
- South Africa
- Spain
- Venezuela
See also
References
External links
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