Global InformationSaab RB05 information
 | Some of this article's listed sources may not be reliable. (March 2018) |
| Saab 305 / RB05 | |
|---|---|
 Board with color print of the SAAB RB05 | |
| Type | Air-to-surface and limited air-to-air |
| Place of origin | Sweden |
| Service history | |
| In service | 1972 – 2005 |
| Used by | Sweden |
| Production history | |
| Manufacturer | Missile – Saab-Scania, Missiles and Electronics Engine – Volvo Flygmotor[1] |
| Specifications | |
| Mass | 305 kg (672 lb) |
| Length | 3.6 m (11.8 ft) |
| Diameter | 0.3 m (11.8 in) |
| Wingspan | 0.8 m (31.5 in) |
| Warhead | 160 kg high explosive |
Detonation mechanism | Proximity fuze |
| Engine | VR 35[a] liquid propellant rocket engine[1] |
Operational range | 9 km (5.6 mi/4.9 nm) |
| Maximum speed | supersonic |
Guidance system | radio controlled manual command to line of sight |
Launch platform | Saab 37 Viggen Saab 105 |
The Saab RB05 (abbreviation of Swedish: robot 05, "missile 05"), initially named Saab 305 (RB 305)[b] or AT 3 internally, was a short-range air-to-surface missile with limited air-to-air capability that was developed in the 1960s by the Swedish company Saab-Scania, Missiles and Electronics for the Swedish Air Force.
- ^ a b Jane's all the world's aircraft 1974-75. Janes Information Group. p. 64. Retrieved 2023-08-27.
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