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Hydrocarbon polymeric binder for advanced solid propellantVarious experimental factors were examined to determine the source of difficulty in an isoprene polymerization in the 5-gallon reactor which gave a non-uniform product of low functionality. It was concluded that process improvements relating to initiator and monomer purity were desirable, but that the main difficulty was in the initiator feed system. A new pumping system was installed and an analog simulation of the reactor, feed system and initiator decomposition kinetics was devised which permits the selection of initial initiator concentrations and feed rates to use to give a nearly uniform initiator concentration throughout a polymerization run. An isoprene polymerization was run in which the process improvements were implemented.
Document ID
19720025117
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Potts, J. E.
(Union Carbide Corp. Bound Brook, NJ, United States)
Ashcraft, A. C., Jr.
(Union Carbide Corp. Bound Brook, NJ, United States)
Wise, E. W.
(Union Carbide Corp. Bound Brook, NJ, United States)
Date Acquired
August 6, 2013
Publication Date
May 15, 1971
Subject Category
Propulsion Systems
Report/Patent Number
NASA-CR-128414
Report Number: NASA-CR-128414
Accession Number
72N32767
Funding Number(s)
CONTRACT_GRANT: JPL-951210
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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