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Kosmos-1
AKA: 11K65;65;8K65;R-14;Skean;SS-5. Status: Active. Thrust: 1,740.02 kN (391,173 lbf). Gross mass: 87,200 kg (192,200 lb). Unfuelled mass: 5,300 kg (11,600 lb). Specific impulse: 292 s. Specific impulse sea level: 248 s. Burn time: 130 s. Height: 22.40 m (73.40 ft). Diameter: 2.40 m (7.80 ft). Span: 4.40 m (14.40 ft).
Cost $ : 10.000 million.
| R-16-1 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. |
Country: Ukraine. Engines: RD-216. Launch Vehicles: R-14, Kosmos 65S3, R-14U, Kosmos 11K65, Kosmos 11K65M, K65M-R, Vertikal' K65UP, K65M-RB. Propellants: Nitric acid/UDMH.
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