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Ignition Problems in Solid-Propellant RocketsMethods of analysis of solid rocket motor ignition and Igniter performance are given. Ignition and ignition Internal ballistic performance are treated beginning with the combustion of the igniter pyrotechnic after the Initiator has functioned. The ignition phenomenon is followed through the (a) igniter ballistic performance, (b) pre-ignition motor port volume pressurization and convective heat transfer (c) motor propellant grain ignition, and (d) subsequent motor ballistics to equilibrium motor operating pressure.
Document ID
19690030797
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
B E Paul (Aerojet-General Corporation Sacramento, California, United States)
R L Lovine (Aerojet-General Corporation Sacramento, California, United States)
Date Acquired
August 5, 2013
Publication Date
August 1, 1968
Publication Information
Publication: Advances in Tactical Rocket Propulsion Conference Proceedings
Publisher: Advisory Group for Aerospace Research and Development (AGARD)
Subject Category
Fluid Mechanics And Thermodynamics
Meeting Information
Meeting: AGARD Colloquium on Progress in Tactical Rocket Propulsion
Location: La Jolla, CA
Country: US
Start Date: April 22, 1965
End Date: April 23, 1965
Sponsors: North Atlantic Treaty Organization
Accession Number
69N40182
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
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IDRelationTitle19690030791Collected WorksAdvances in Tactical Rocket Propulsion Conference ProceedingsN69-40176 24-28Collected Works
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