NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Solid rocket propellant waste disposal/ingredient recovery studyA 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.
Document ID
19760019263
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Mcintosh, M. J.
(Thiokol Chemical Corp. Brigham City, UT, United States)
Date Acquired
September 3, 2013
Publication Date
May 4, 1976
Subject Category
Propellants And Fuels
Report/Patent Number
MER-1374A
NASA-CR-148195
Accession Number
76N26351
Funding Number(s)
CONTRACT_GRANT: JPL-954161A
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available