Composite propellant combustion
- 1 August 1970
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 8 (8), 1488-1491
- https://doi.org/10.2514/3.5928
Abstract
No abstract availableKeywords
This publication has 10 references indexed in Scilit:
- A technique for controlling the position of a burning solid-propellant sample in a combustion bombJournal of Spacecraft and Rockets, 1969
- Combustion of ammonium perchlorate - Some negative conclusions.AIAA Journal, 1968
- Effect of surface reactions on the solid propellant response function.AIAA Journal, 1968
- Experimental techniques for solid-propellant combustion research.AIAA Journal, 1967
- A DETAILED MODEL OF THE COMBUSTION OF COMPOSITE SOLID PROPELLANTSPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1967
- INVESTIGATION OF SOLID PROPELLANT DECOMPOSITION CHARACTERISTICS AND THEIR RELATION TO OBSERVED BURNING RATESPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1967
- A Model of Composite Propellant Combustion Including Surface Heterogeneity and Heat GenerationAIAA Journal, 1966
- A study of composite solid-propellant flame structure using a spectral radiation shadowgraph techniqueAIAA Journal, 1965
- Measurement of temperature profiles through solid-propellant flames using fine thermocouplesAIAA Journal, 1965
- Burning Mechanism of Ammonium Perchlorate PropellantsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1960