Cast composite solid propellants with different combustion stabilizers

Cast composite solid propellants with different combustion stabilizers

The effect of four different compounds as the combustion stabilizers of composite solid propellants based on the AP/HTPB/IPDI has been presented in this paper. Except that, various total solid content, ammonium-perchlorate bimodal and trimodal combination of particle sizes ratio have been made by pr...

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Bibliographic Details
Main Authors: Rodić Vesna, Dimić Mirjana, Brzić Saša, Gligorijević Nikola
Format: Article
Language:English
Published: Military Technical Institute, Belgrade 2015-01-01
Series:Scientific Technical Review
Subjects:
composite solid propellant
composite rocket propellant
cast propellant
combustion stability
stabilizers
aluminium
zirconium carbide
titanium oxide
antimony oxide
temperature sensitivity
burning rate
Online Access:https://scindeks-clanci.ceon.rs/data/pdf/1820-0206/2015/1820-02061502003R.pdf

Internet

https://scindeks-clanci.ceon.rs/data/pdf/1820-0206/2015/1820-02061502003R.pdf

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