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NASA NTRS · 19680026257

An evaluation of aft-end ignition for solid propellant rocket motors

Abstract

Performance evaluation of solid propellant rocket motor ignition to determine igniter design and parameters to avoid overpressurization

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BibTeXRIS

Fitch, R. E., Guenther, J. L., Kilgroe, J. D.. 1968-09-01. An evaluation of aft-end ignition for solid propellant rocket motors. https://ntrs.nasa.gov/citations/19680026257

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