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SS-X-10 'Scrag' Universal |
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SS-X-10 'Scrag' Universal |
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SS-X-10 'Scrag' Ballistic Missile |
Designer - V. N. Chelomei |
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Manufacturer: |
OKB-52 |
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Role: |
Universal Rocket System |
| Soviet Designation: | GR-1 and UR-200 |
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Year Adopted: |
Never entered service |
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Operational Status: |
Russia - Experimental only. Was cancelled in 1964 before deployment. |
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Warheads: |
A single 5 or 15 Megaton warhead |
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Engine: |
RD-204 (1st stage) |
| Fuel: | Liquid Oxygen, Kerosene, Nitrogen Tetroxide |
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Length: |
__ feet (34.65 meters) |
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Width: |
__ feet (10 meters) |
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Weight at Launch: |
138 tons |
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Launch Type: |
Hot Launched, Soft Site Based |
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Range: |
1400 kilometers (___ miles) |
| CEP (Circular Probability of Error): | 1800 to 5500 meters (___ feet) |
| The SS-X-10 'Scrag' in Pictures |
Development, History, and Use |
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