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Titolo:
Propellant formulation factors and metal agglomeration in combustion of aluminized solid rocket propellant
Autore:
Babuk, VA; Vassiliev, VA; Sviridov, VV;
Indirizzi:
Balt State Tech Univ, St Petersburg, Russia Balt State Tech Univ St Petersburg Russia h Univ, St Petersburg, Russia
Titolo Testata:
COMBUSTION SCIENCE AND TECHNOLOGY
, volume: 163, anno: 2001,
pagine: 261 - 289
SICI:
0010-2202(2001)163:<261:PFFAMA>2.0.ZU;2-Q
Fonte:
ISI
Lingua:
ENG
Keywords:
composite solid propellant; combustion; agglomeration; ammonium perchlorate; ammonium dinitramide;
Tipo documento:
Article
Natura:
Periodico
Settore Disciplinare:
Engineering, Computing & Technology
Citazioni:
28
Recensione:
Indirizzi per estratti:
Indirizzo: Babuk, VA Balt State Tech Univ, St Petersburg, Russia Balt State Tech Univ St Petersburg Russia Petersburg, Russia
Citazione:
V.A. Babuk et al., "Propellant formulation factors and metal agglomeration in combustion of aluminized solid rocket propellant", COMB SCI T, 163, 2001, pp. 261-289

Abstract

An experimental study of aluminized solid rocket propellant combustion wasconducted in order to determine the influence of various propellant formulation factors on metal agglomeration, The results allowed us to determine the dependencies of the agglomeration process characteristics on the physical and mechanical properties of the propellant binder, the particle size of the metal fuel, the type of film covering the original metal particles, andthe type of oxidizer in the propellant. These results, combined with earlier data, were used to develop a physical picture of the agglomeration process, which may serve as the basis for conducting analysis of the influence of various propellant formulation factors on agglomeration.

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Documento generato il 23/09/20 alle ore 15:58:28