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
1968-01-15
Report
No indication
English
Rapid Depressurization Dynamics of Solid Propellant Rocket Motors AIAA Paper
British Library Conference Proceedings | 2007
|Combustion instability in solid propellant rocket motors
Engineering Index Backfile | 1958
|