Calculation of solid propellant burning rates from condensed-phase decomposition kinetics
Authors:
- 20 January 1969
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- Surface temperature of deflagrating ammonium perchlorate crystals.AIAA Journal, 1967
- INVESTIGATION OF SOLID PROPELLANT DECOMPOSITION CHARACTERISTICS AND THEIR RELATION TO OBSERVED BURNING RATES1967
- A Model of Composite Propellant Combustion Including Surface Heterogeneity and Heat GenerationAIAA Journal, 1966
- Measurement of temperature profiles through solid-propellant flames using fine thermocouplesAIAA Journal, 1965
- A Differential Scanning Calorimeter for Quantitative Differential Thermal Analysis.Analytical Chemistry, 1964
- DISSOCIATION PRESSURE OF AMMONIUM PERCHLORATE1The Journal of Physical Chemistry, 1963
- Burning Mechanism of Ammonium Perchlorate Propellants1960