3 edition of Solid-propellant rocket motor internal ballistics performance variatio analysis (phase five) found in the catalog.
Solid-propellant rocket motor internal ballistics performance variatio analysis (phase five)
by Engineering Experiment Station, Auburn University, National Aeronautics and Space Administration, National Technical Information Service, distributor in Auburn, Ala, [Washington, DC, Springfield, Va
Written in English
|Other titles||Solid propellant rocket motor internal ballistics performance variatio analysis (phase five)|
|Statement||by Richard H. Sforzini and Jesse E. Murph|
|Series||NASA contractor report -- NASA CR-177145|
|Contributions||Murph, Jesse E, United States. National Aeronautics and Space Administration|
|The Physical Object|
Sinai and the Monastery of St. Catherine
Transactions of the National Association for the Promotion of Social Science, Huddersfield meeting, 1883.
Made in Czechoslovakia
The littlest fire truck
Development funds 1996/97.
From letter to publication
War law service
Records of Inverness
Painting in watercolor
Get this from a library. Solid-propellant rocket motor internal ballistics performance variatio analysis (phase five): final report. [Richard H Sforzini; Jesse E Murph; United States. National Aeronautics and Space Administration.].
Full text of "NASA Technical Reports Server (NTRS) Study of solid rocket motor for space shuttle booster, Volume 3: Program acquisition planning" See other formats.
Solid rocket motor system design is a typical example of multidisciplinary analysis, design and optimization process, and encompasses modules for grain, nozzle, internal ballistics, combustion Author: Alain Davenas.
Regression rate data from preliminary motor firings at moderate oxidizer mass fluxes ( g/cm2-s) agree well with literature after accounting for the effects of motor scale. The lab-scale hybrid.
L = 45, Operating principle ~specific impulse of a rocket ~internal ballistics ~rocket p erformance considerations ~solid propellant rockets ~selection criteria of solid propellants ~propellant grain design considerations ~erosive burning in solid r ockets ~liquid propellant rockets ~selection of liquid propellants ~various feed systems for.
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