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NASA NTRS · 19720025117

Hydrocarbon polymeric binder for advanced solid propellant

Abstract

Various 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.

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BibTeXRIS

Potts, J. E., Ashcraft, A. C., Jr., Wise, E. W.. 1971-05-15. Hydrocarbon polymeric binder for advanced solid propellant. https://ntrs.nasa.gov/citations/19720025117

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