Conservation equations coupled with mass balance equation to produce method of computing transient burning rates in solid propellant motors
A theoretical study of combustion and quenching of solid propellant rocket motors during depressurization
15.01.1968
Report
Keine Angabe
Englisch
Rapid Depressurization Dynamics of Solid Propellant Rocket Motors AIAA Paper
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Engineering Index Backfile | 1958
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