NASA NTRS · 19740011276
Solid Propellant Grain Structural Integrity Analysis
Abstract
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.
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1973-06-01. Solid Propellant Grain Structural Integrity Analysis. https://ntrs.nasa.gov/citations/19740011276
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