NASA NTRS · 19700064776
Characteristics of solid propellant motor aft- end ignition
Abstract
Aft-end igniter design and placement for solid propellant rocket motors avoiding overpressurization and nozzle pressure oscillations
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Fitch, R. E., Kilgroe, J. D.. 1970-07-01. Characteristics of solid propellant motor aft- end ignition. https://ntrs.nasa.gov/citations/19700064776
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