NASA NTRS ยท 19760019263
Solid rocket propellant waste disposal/ingredient recovery study
Abstract
A comparison of facility and operating costs of alternate methods shows open burning to be the lowest cost incineration method of waste propellant disposal. The selection, development, and implementation of an acceptable alternate is recommended. The recovery of ingredients from waste propellant has the probability of being able to pay its way, and even show a profit, when large consistent quantities of composite propellant are available. Ingredients recovered from space shuttle waste propellant would be worth over $1.5 million. Open and controlled burning are both energy wasteful.
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Mcintosh, M. J.. 1976-05-04. Solid rocket propellant waste disposal/ingredient recovery study. https://ntrs.nasa.gov/citations/19760019263
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