Erosive effect is greater in slow burning propellants than in fast burning ones; existence of apparent "threshold velocity for erosion" is tentatively attributed to failure of onedimensional idealization to represent true flow conditions obtaining at fore end of grain; more comprehensive studies of phenomenon required in order to resolve threshold velocity question. (formerly Am Rocket Soc -- J)
Erosive burning of some composite solid propellants
Jet Propulsion
Jet Propulsion ; 24 , n 1
1954
Aufsatz (Zeitschrift)
Englisch
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EROSIVE BURNING OF SOLID PROPELLANTS
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