| RSD-10 Pioneer SS-20 Saber | |
|---|---|
| Type | Intermediate-range ballistic missile |
| Place of origin | Soviet Union |
| Service history | |
| In service | 1976–1988 |
| Used by | Soviet Strategic Rocket Forces |
| Production history | |
| Designer | Moscow Institute of Thermal Technology |
| Manufacturer | Votkinsk Machine Building Plant |
| Specifications | |
| Weight | 37,100 kg (82,000 lb) |
| Length | 16.5 m (54 ft) |
| Diameter | 1.8 m (5 ft 11 in) |
| Warhead | Three 150 kT MIRVs |
| Engine | Two-stage solid propellant |
| Operational range | 5,500 km (3,400 mi) |
| Guidance system | Inertial |
| Accuracy | 150-450 m CEP |
| Launch platform | Road-mobile TEL |
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