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)
1980 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|
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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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