R.650 (missile): Difference between revisions
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Latest revision as of 18:03, 10 March 2019
| R.650 | |
|---|---|
| File:Superbvrmissile.png R.650C | |
| Type | Long-range air-to-air missile |
| Place of origin | Sieuxerr |
| Service history | |
| In service | 1989-Present |
| Used by | Sieuxerr |
| Production history | |
| Designer | MBDA |
| Designed | 1985-1988 |
| Manufacturer | MBDA |
| Produced | 1989 |
| Variants | R.650A R.650B R.650C |
| Specifications | |
| Weight | 375 kg |
| Length | 3.75 m |
| Diameter | 285 mm |
| Warhead | Annular blast-fragmenting warhead |
| Warhead weight | 55 kg |
Detonation mechanism | Proximity fuze |
| Engine | 2 stage booster rocket/ramjet |
| Wingspan | 550 mm |
| Propellant | Solid fuel |
Operational range | 200+ km |
| Speed | Mach 4.5 |
Guidance system | Semi-active and active radar homing with mid-course updates |
Launch platform | Aircraft |
The R.650 Air-to-air missile is a long-range missile used mostly by the Sieuxerrian Air Force and Sieuxerrian Navy. Its primary mission is to intercept long-range bomber aircraft, cruise missiles, and anti-shipping missiles.