NASA NTRS · 19720025093
Hydrocarbon polymeric binder for advanced solid propellant
Abstract
The results of curing vinyl alcohol terpolymers of ethylene, propylene and vinyl acetate are reported for an average functionality of 1.24 when reacted with an equivalent amount of diisocynate, and saturated polyisoprene derivative is described having terminal methyl ester functionality. The development is reported of two hydroxy-telechelic polyisoprenes prepared by DEAB initiated free radical polymerization followed by LiAlH4 reduction of the end groups.
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Potts, J. E., Ashcraft, A. C., Jr., Wise, E. W.. 1971-12-31. Hydrocarbon polymeric binder for advanced solid propellant. https://ntrs.nasa.gov/citations/19720025093
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