Solid-propellant rocket motor internal ballistics performance variatio analysis (phase five)
Subtitle: final report
By: by Richard H. Sforzini and Jesse E. Murph.
Contributors: Murph, Jesse E.; United States. National Aeronautics and Space Administration.
Series: NASA contractor report -- NASA CR-177145.
Publisher: Engineering Experiment Station, Auburn University; National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1980
Place of publication: Auburn, Ala; [Washington, DC; Springfield, Va
Language: eng
Format: Microform
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.
Other titles: Solid propellant rocket motor internal ballistics performance variatio analysis (phase five)
Notes: Distributed to depository libraries in microfiche.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1986] 1 microfiche.