Increasing the burning rate of nitramine modified double-base propellant with ACP

Tuijin Jishu/Journal of Propulsion Technology

Volumn 26, Issue 1, 2005, Pages 84-88

  Liao, Lin Quan ^a   Qin, Guang Ming ^a   Li, Xiao Jiang ^a   Wang, Guo Qiang ^a   Li, Jun Qiang ^a  

^a XI'AN MODERN CHEMISTRY RESEARCH INSTITUTE   (China)

Author keywords

Burning rate; Combustion performance; High burning rate propellant; Modified double base propellant

Indexed keywords

COMBUSTION; FLAME RESEARCH; MEASUREMENTS; MODIFICATION; ORGANIC COMPOUNDS; SURFACES;

BURNING RATE; COMBUSTION PERFORMANCE; HIGH BURNING RATE PROPELLANT; MODIFIED DOUBLE BASE PROPELLANT;

PROPELLANTS;

EID: 15944415817     PISSN: 10014055     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (7)

1. Fogelzang A E, Denisyuk A P. Burning behavior of composite propellants with fast-burning inclusions[J]. Propulsion, 1998, 16(2): 374-376.
2. Fogelzang A E, Pimenov A Yu, Denisyuk A P. Mechanism of modifying ballistic properties of propellant formulations by fast-burning inclusions[J]. Defence Science, 1998, 48(4): 357-364.
3. GUO Wan-dong, WANG Ke, DING Wen-xia. Study of increasing the burning rate of solid propellants by adding fast burning energetic materials[J]. Journal of Propulsion Technology, 1998, 19(3).
4. YANG Rong-jie. A survey of development of porous solid propellants with ultra-high burning rate[J]. Journal of Propulsion Technology, 1992, 13(4).