Propulsion Spreadsheet

Propulsion Spreadsheet - 49.3 8.31 178000 12125 3.25 0.779...

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Rocket Propulsion Market Survey (final results based upon preliminary payload estimate) CEV Payload to LEO Rocket Name Height (m)Diameter (m) Mass (kg) Payload to LEO Thrust (MN) 35000 Stage 1 Stage 2 Stage 3 Sum Saturn V 111 10 2900000 118000 33.4 5 1 39.4 Titan II 28.6 3 120000 3750 2.1 0.44 0 2.54 Required Total Thrust Vostok 38.36 8 308600 4725 3.88 0.912 0.0545 4.8465 (MN) Voskhod 44.42 8 298400 5900 3.981 0.941 0.294 5.216 13.197903 Soyuz
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Unformatted text preview: 49.3 8.31 178000 12125 3.25 0.779 0.298 4.327 Sources: http://en.wikipedia.org/wiki/Crew_Exploration_Vehicle http://en.wikipedia.org/wiki/Saturn_V http://en.wikipedia.org/wiki/Vostok_rocket http://en.wikipedia.org/wiki/Titan_%28rocket%29 http://en.wikipedia.org/wiki/Soyuz_launch_vehicle http://en.wikipedia.org/wiki/Voskhod_rocket Saturn V...
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