Solid propellant grain design and internal ballistics, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical)

NASA/SP-8076, Solid propellant grain design and internal ballistics, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical), NASA Lewis Research Center (Cleveland, OH, United States), March,1972, pp. 110, Format(s): PDF 6701k

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The ballistic aspects of grain design were studied to outline the steps necessary to achieve a successful grain design. The relationships of the grain design to steady-state mass balance anderosive burning are considered. Grain design criteria is reviewed, and recommended design criteria are included.

Keywords:	propellants, interior ballistics, propellant grains, solid rocket propellants, engine design, optimization, rocket engines, systems engineering
CASI Document ID Number:	73N15804
Subjects:	Chemistry and Materials: Propellants and Fuels: Solid Propellants
ID Code:	120
Deposited On:	23 May 2002