NASA NTRS · 19660055159
The ignition transient in solid propellant rocket motors.
Abstract
Ignition pressure transient of rocket motor, discussing initial ignition event, flame spreading and final chamber filling, convective heating effect on burning rate, etc
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Most, W. J., Parker, K. H., Summerfield, M.. 1966-06-01. The ignition transient in solid propellant rocket motors.. https://ntrs.nasa.gov/citations/19660055159
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