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Liquid rocket engine turbopump shafts and couplings, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical)

NASA/SP-8101, Liquid rocket engine turbopump shafts and couplings, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical), NASA Lewis Research Center (Cleveland, OH, United States), September,1972, pp. 130, Format(s): PDF 13343k

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Design criteria and recommended practices are presented for designing tubopump shafts and couplings. Design parameters, material selection, and structural analysis are discussed.
Keywords:propulsion systems, engine design, liquid propellant rocket engines, shafts (machine elements), turbine pumps, bearings, fatigue life, mechanical properties, reliability engineering, structural analysis, temperature gradients
CASI Document ID Number:74N14441
Subjects:Astronautics: Spacecraft Propulsion And Power: Rocket Engines, Nozzles And Thrust Chambers
ID Code:130
Deposited On:23 May 2002