NASA NTRS · 19660039873
Gas evolution from a solid rocket propellant during depressurization to produce a quench.
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.. 1966-01-01. Gas evolution from a solid rocket propellant during depressurization to produce a quench.. https://ntrs.nasa.gov/citations/19660039873
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