Mass flow rate of gas evolution from burning solid rocket propellant during transient depressurization of combustion chamber
Gas evolution from a solid rocket propellant during depressurization to produce a quench.
1966-01-01
Sonstige
Keine Angabe
Englisch
Rapid Depressurization Dynamics of Solid Propellant Rocket Motors AIAA Paper
British Library Conference Proceedings | 2007
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