Effect of ammonium oxalate/strontium carbonate on the burning rate characteristics of composite propellants

Journal of Thermal Analysis and Calorimetry

Volumn 86, Issue 2, 2006, Pages 497-503

  Sun, Y L ^a   Li, S F ^a   Ding, D H ^b  

^a UNIVERSITY OF SCIENCE AND TECHNOLOGY OF CHINA   (China)

^b CSSG Chemical Power Technological Research Institute   (China)

Author keywords

Burning rate characteristic; Composite propellants; TG DTG

Indexed keywords

BURNING RATE CHARACTERISTICS; COMPOSITE PROPELLANTS; SYNERGETIC EFFECTS; TEMPERATURE SENSITIVITY;

AMMONIUM COMPOUNDS; COMBUSTION; COMPOSITE MATERIALS; DECOMPOSITION; FOURIER TRANSFORM INFRARED SPECTROSCOPY;

PROPELLANTS;

EID: 33750031790     PISSN: 13886150     EISSN: None     Source Type: Journal    
DOI: 10.1007/s10973-005-7386-0     Document Type: Article

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