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Kosmos A-1
AKA: 11K63;63;8K63;R-12;Sandal;SS-4. Status: Out of production. Thrust: 730.50 kN (164,223 lbf). Gross mass: 39,515 kg (87,115 lb). Unfuelled mass: 3,150 kg (6,940 lb). Specific impulse: 264 s. Specific impulse sea level: 230 s. Burn time: 125 s. Height: 18.00 m (59.00 ft). Diameter: 1.60 m (5.20 ft). Span: 1.80 m (5.90 ft).
Cost $ : 4.500 million.
| DF-2A-1 Nitric acid/kerosene rocket stage. 300.00 kN (67,443 lbf) thrust. Mass 30,000 kg (66,139 lb). |
| R-16-2 Nitric acid/UDMH propellant rocket stage. Range 12,000 km. TsNIIMash has 1:10 structural simulation model. Two stage ICBM with nitric acid oxidizer. Developed 1956-1961. Entered service 1961. Chief designer Yangel. Source: Placard, TsNIIMash. |
| DF-2-1 Nitric acid/kerosene rocket stage. 300.00 kN (67,443 lbf) thrust. Mass 30,000 kg (66,139 lb). |
Country: Ukraine. Engines: RD-214, RD-215. Launch Vehicles: Kosmos 63S1, Kosmos 11K63, Kosmos 63S1M. Propellants: Nitric acid/Kerosene.
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