Regarding the evaluation of the solid rocket propellant response function to pressure coupling

Regarding the evaluation of the solid rocket propellant response function to pressure coupling

High frequency combustion instabilities imply a major risk for the solid rocket motor stableworking and they are directly linked to the propellant response to chamber pressure coupling. Thisarticle discusses a laboratory testing method for the measurement and evaluation of the pressurecoupled respon...

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Bibliographic Details
Main Authors:	Ioan ION, Titica VASILE, Doru SAFTA
Format:	Article
Language:	English
Published:	National Institute for Aerospace Research “Elie Carafoli” - INCAS 2011-03-01
Series:	INCAS Bulletin
Subjects:	solid rocket propellant response testing method motor chamber
Online Access:	http://bulletin.incas.ro/files/doru_safta_v3is1_full.pdf

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