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Suppressants for lowering propellant binder burning rateAddition of boron compound to lower burning rate of solid propellant binder is reported. Chemical reactions involved in propellant binder modification are described. Advantages of method for lowering burning rate are analyzed.
Document ID
19720000559
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Thompson, W. W. (Rocketdyne)
Date Acquired
August 6, 2013
Publication Date
September 1, 1972
Subject Category
Materials
Report/Patent Number
ARC-10563
Report Number: ARC-10563
Accession Number
72B10560
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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