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Burning Mechanism of Aluminized Solid Rocket Propellants Based on Energetic Binders
Author(s) -
Babuk Valery A.,
Dolotkazin Ildar N.,
Glebov Andrey A.
Publication year - 2005
Publication title -
propellants, explosives, pyrotechnics
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.56
H-Index - 65
eISSN - 1521-4087
pISSN - 0721-3115
DOI - 10.1002/prep.200500012
Subject(s) - propellant , solid fuel rocket , rocket (weapon) , mechanism (biology) , combustion , materials science , energetic material , aerospace engineering , rocket propellant , nuclear engineering , composite material , forensic engineering , engineering , explosive material , physics , chemistry , organic chemistry , quantum mechanics
This paper reports results obtained from an experimental study of the combustion mechanism of aluminized propellants based on an energetic binder. The techniques used in this investigation include:
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