Solid propellant grain structural integrity analysis, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical)

NASA/SP-8073, Solid propellant grain structural integrity analysis, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical), NASA Lewis Research Center (Cleveland, OH, United States), June,1973, pp. 114, Format(s): PDF 6357k

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The structural properties of solid propellant rocket grains were studied to determine the propellant resistance to stresses. Grain geometry, thermal properties, mechanical properties, and failure modes are discussed along with design criteria and recommended practices.

Keywords:	propellants, propellant grains, solid rocket propellants, structural analysis, failure analysis, mechanical properties, thermodynamic properties
CASI Document ID Number:	74N19389
Subjects:	Chemistry and Materials: Propellants and Fuels: Solid Propellants
ID Code:	146
Deposited On:	23 May 2002