Combustion wave structures of ammonium perchlorate composite propellants
- 1 July 1986
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Propulsion and Power
- Vol. 2 (4), 296-300
- https://doi.org/10.2514/3.22885
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Combustion of RDX/AP composite propellants at low pressuresJournal of Spacecraft and Rockets, 1984
- Physicochemical processes of HMX propellant combustionSymposium (International) on Combustion, 1982
- A model of composite solid-propellant combustion based on multiple flamesAIAA Journal, 1970
- Contribution of solid-phase heat release to AP composite-propellant burning rate.AIAA Journal, 1968
- 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