Study of increasing the burning rate of solid propellants by adding fast burning energetic materials

Tuijin Jishu/Journal of Propulsion Technology

Volumn 19, Issue 3, 1998, Pages 86-93

  Guo, Wandong ^a   Wang, Ke ^a   Ding, Wenxia ^a  

^a Hubei Red Star Chemical Research Institute   (China)

Author keywords

Burning rate modifier; Combustion performance; High burning rate propellant; Hydroxy terminated polybutadiene propellant

Indexed keywords

COMBUSTION; FLAME RESEARCH; REACTION KINETICS;

BURNING RATE MODIFIER; HIGH BURNING RATE PROPELLANT; HYDROXY TERMINATED POLYBUTADIENE PROPELLANTS;

SOLID PROPELLANTS;

EID: 0032307878     PISSN: 10014055     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (3)

1. Sayles D C. Embedded explosives as burning rate accelerators for solid propellants. U. S. P. 5015310, 1991.
2. Fogelzang A E. Mechanism of modifying ballistic properties of propellant formulations by fast-burning inclusions. Mendeleev University of Chemical Technology, Russia, 1997.