NASA/TP-3589, Herda, D.A. and Gross*, R.S., High Pressure Oxidizer Turbopump (HPOTP) Inducer Dynamic Design Environment, Structures and Dynamics Laboratory, Science and Engineering Directorate. NASA Marshall Space Flight Center, AL 35812 and *Auburn University, November 1995, pp. 27, Format(s): PDF 351k |
The dynamic environment must be known to evaluate high pressure oxidizer turbopump inducer fatigue life. This report sets the dynamic design loads for the alternate turbopump inducer as determined by water-flow rig testing. Also, guidelines are given for estimating the
dynamic environment for other inducer and impeller applications.
| Keywords: | inducer, fatigue life, alternate turbopump, high pressure oxidizer turbopump, space shuttle main engine |
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| CASI Document ID Number: | 96N19293 |
| Subjects: | Engineering: Structural Mechanics: Stresses and Loads |
| ID Code: | 295 |
| Deposited On: | 27 June 2002 |