Solid-propellant rocket motor internal ballistics performance variatio analysis (phase five) [microform] : final report / by Richard H. Sforzini and Jesse E. Murph.

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Bibliographic Details
Main Author:	Sforzini, Richard H.
Corporate Author:	United States. National Aeronautics and Space Administration
Other Authors:	Murph, Jesse E.
Other title:	Solid propellant rocket motor internal ballistics performance variatio analysis (phase five)
Format:	Government Document Microfilm Book
Language:	English
Published:	Auburn, Ala. : [Washington, DC] : [Springfield, Va.] : Engineering Experiment Station, Auburn University ; [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], [1980]
Series:	NASA contractor report ; NASA CR-177145.
Subjects:	Applications programs (Computers) Booster rocket engines. Burning rate. Combustion stability. Interior ballistics. Rocket engine design. Rocket thrust. Solid propellant combustion. Solid propellant rocket engines. Space shuttle boosters. Thrust distribution. Ballistics, Interior.

Norlin Library - Government Information - Microform

Holdings details from Norlin Library - Government Information - Microform
Call Number:	NAS 1.26:177145
NAS 1.26:177145	Restricted Place a Hold