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Space shuttle main engine structural analysis and data reduction/evaluation. Volume 2, High pressure oxidizer turbo-pump turbine end bearing analysis : final report / by Gregory A. Sisk.
Connect to full text Available online
View online- Format:
- Book
- Government document
- Author/Creator:
- Sisk, Gregory A., author.
- Series:
- NASA contractor report ; NASA CR-183664.
- [NASA contractor report] ; NASA-CR-183664
- Language:
- English
- Subjects (All):
- Data reduction.
- Finite element method.
- Space shuttles--Propulsion systems.
- Space shuttles.
- Structural analysis (Engineering).
- Turbine pumps.
- Synthetic training devices.
- structural analysis.
- Physical Description:
- 1 online resource (approximately 85 pages) : illustrations.
- Other Title:
- High pressure oxidizer turbo-pump turbine end bearing analysis
- Place of Publication:
- Huntsville, AL : Lockheed Missiles & Space Company, Huntsville Engineering Center, 1989.
- Notes:
- Description based on online resource, PDF version; title from title page (NTRS, viewed March 10, 2022).
- "April 1989."
- "LMSC-HEC TR F268584-II."
- Includes bibliographical reference (page 6).
- Other Format:
- Microfiche version: Sisk, Gregory A. Space shuttle main engine structural analysis and data reduction/evaluation. Volume 2, High pressure oxidizer turbo-pump turbine and bearing analysis.
- Print version: Sisk, Gregory A. Space shuttle main engine structural analysis and data reduction/evaluation. Volume 2, High pressure oxidizer turbo-pump turbine end bearing analysis.
- OCLC:
- 1305016322
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