NASA NTRS · 19650031864
An experimental investigation of gas evolution from a solid rocket propellant during pressure transients.
Abstract
Mass flow rate of gas evolution from burning solid rocket propellant during transient depressurization of combustion chamber
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Bunde, G. W., Fletcher, E. A.. 1965-01-01. An experimental investigation of gas evolution from a solid rocket propellant during pressure transients.. https://ntrs.nasa.gov/citations/19650031864
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