NASA/SP-8121, Burcham, R.E., Liquid rocket engine turbopump rotating-shaft seals, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical), NASA Lewis Research Center (Cleveland, OH, United States) and Rockwell International Corp. (Canoga Park, CA, United States), February,1978, pp. 160, Format(s): PDF 16574k |
A monograph is organized and presents, for effective use in design, the significant experience and knowledge accumulated in development and operational programs to date. It reviews and assesses current practices, and from them establishes firm guidance for achieving greater consistency in design, increased reliability in the end product, and greater efficiency in the design effort. The monograph is divided into two major sections: state of the art and design criteria.
| Keywords: | mechanical engineering, leakage, seals (stoppers), systems engineering, turbine pumps, liquid propellant rocket engines, sealing, shafts (machine elements) |
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| CASI Document ID Number: | 78N30584 |
| Subjects: | Engineering: Mechanical Engineering: Seals |
| ID Code: | 191 |
| Deposited On: | 10 June 2002 |