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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Manylion Llyfryddiaeth

Prif Awduron:	Rodić Vesna, Dimić Mirjana, Brzić Saša, Gligorijević Nikola
Fformat:	Artigo
Iaith:	Inglês
Cyhoeddwyd:	Military Technical Institute, Belgrade 2015-01-01
Cyfres:	Scientific Technical Review
Pynciau:	composite solid propellant composite rocket propellant cast propellant combustion stability stabilizers aluminium zirconium carbide titanium oxide antimony oxide temperature sensitivity burning rate
Mynediad Ar-lein:	https://scindeks-clanci.ceon.rs/data/pdf/1820-0206/2015/1820-02061502003R.pdf
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