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Credit: © Mark Wade. 5,802 bytes. 16 x 108 pixels.
Family: UR. Country: Russia. Status: Hardware. Other Designations: RS-18. Department of Defence Designation: SS-19 Mod.1. Article Number: 15A30. Manufacturer's Designation: UR-100N.
Launch vehicle based decommissioned Ukrainian ICBMs, but built by Russia's NPO MASH. 106 tonne liftoff mass.
LEO Payload: 1,700 kg. to: 200 km Orbit. at: 74.0 degrees. Liftoff Thrust: 190,000 kgf. Total Mass: 104,000 kg. Core Diameter: 2.5 m. Total Length: 26.7 m. Launch Price $: 10.50 million.
- Stage Number: 1. 1 x UR-100N Stage 1N Gross Mass: 77,150 kg. Empty Mass: 5,695 kg. Thrust (vac): 181,373 kgf. Isp: 310 sec. Burn time: 121 sec. Isp(sl): 285 sec. Diameter: 2.5 m. Span: 2.5 m. Length: 17.2 m. Propellants: N2O4/UDMH No Engines: 4. RD-0232
- Stage Number: 2. 1 x UR-100N Stage 2N Gross Mass: 12,195 kg. Empty Mass: 1,485 kg. Thrust (vac): 21,850 kgf. Isp: 322 sec. Burn time: 183 sec. Diameter: 2.5 m. Span: 2.5 m. Length: 3.9 m. Propellants: N2O4/UDMH No Engines: 1. RD-0235
|ICBM-Derived LVs - The range of launch vehicles derived from decommissioned ballistic missiles offered for sale by Russia after the cold war.|
Credit: Mark Wade. 41,348 bytes. 640 x 444 pixels.
- 193 - Placard, TsNIIMASH Museum, .
- 455 - Isakowitz, Steven J,, International Reference to Space Launch Systems Third Edition, AIAA, Washington DC, 2000.
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Last update 12 March 2001.
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