NASA NTRS · 19770010200
Solid propellant rocket motor and method of making same
Abstract
A method is described for making a solid propellant rocket motor having a specific concavity formed within the fuel charge. A mandrel with an aperature wider than that of the casing is inserted within the motor casing and a solidifiable propellant cast above the mandrel. The mandrel is removed after the propellant is cured.
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Thibodaux, J. G., Jr., Lewis, D. J.. 1977-01-04. Solid propellant rocket motor and method of making same. https://ntrs.nasa.gov/citations/19770010200
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