NASA NTRS · 19720013112
Demonstration of a sterilizable solid rocket motor system, addendum
Abstract
Technical emphasis was placed on characterization of a scaled-up batch of the improved propellant formulation and determination of the effects of dry heat sterilization on propellant integrity and structural response. The grain stress analysis was directed toward tailoring a fully-bonded grain to the calculated propellant allowable stresses and investigating various bond release concepts to relieve stresses incurred in thermal shrinkage following sterilization.
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Depree, D. O., Lambert, W. L.. 1971-12-01. Demonstration of a sterilizable solid rocket motor system, addendum. https://ntrs.nasa.gov/citations/19720013112
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