This volume brings together the world's most highly regarded scientists in the field of solid rocket propulsion. Thirty-nine papers present in-depth coverage on a wide range of topics including: advanced materials and nontraditional formulations; the chemical aspects of organic and inorganic components in relation to decomposition mechanisms, kinetics, combustion, and modeling; safety issues, hazards and explosive characteristics; and experimental and computational interior ballistics research, including chemical information and the physics of the complex flowfield.
Burning Rate Characteristics of Glycidyl Azide Polymer (GAP) Fuels and Propellants
2000-01-01
10 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
Glycidyl azide polymer combustion modeling
AIAA | 2001
|Reactivity of Azide Polymer Propellants
AIAA | 2000
|Burning rate characteristics of GAP propellants
AIAA | 1990
|Burning rate characteristics of GAP propellants
AIAA | 1988
|Historical development of glycidyl azide polymer
AIAA | 1992
|