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 |
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 |
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| 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 |