SRM internal flow test and computational fluid dynamic analyses [microform] : final report : contract NAS8-39095 / prepared by ERC, Incorporated.

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Bibliographic Details
Corporate Author:	United States. National Aeronautics and Space Administration
Other title:	SRM internal flow tests and computational fluid dynamic analysis : final report. Major task summaries. RSRM full scale motor analyses. Titan, ASRM, and subscale motor analyses. Cold flow analyses and CFD analysis capability development.
Format:	Government Document Microfilm Book
Language:	English
Published:	Huntsville, AL : [Washington, DC] : [Springfield, Va.] : ERC, Inc. ; [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], [1995-]
Series:	NASA contractor report ; NASA CR-201148. NASA contractor report ; NASA CR-203931. NASA contractor report ; NASA CR-203932. NASA contractor report ; NASA CR-203933.
Subjects:	Cold flow tests. Computational fluid dynamics. Ejection. Flow velocity. Inlet temperature. Internal flow. Nozzle efficiency. Nozzle geometry. Nozzle thrust coefficients. Performance tests. Propellant grains. Propellants. Propulsion system performance. Slags. Solid propellant combustion. Solid propellant ignition. Solid propellant rocket engines. Space shuttle boosters. Stress analysis. Titan 4 launch vehicle.

Norlin Library - Government Information - Microform