The Ignition of Ultra-Fine Aluminum in Ammonium Perclorate Solid Propellant Flames
- 26 June 2003
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Combustion Mechanisms of Bimodal and Ultra-Fine Al in AP Solid PropellantsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2002
- The effects of bimodal aluminum with ultrafine aluminum on the burning rates of solid propellantsProceedings of the Combustion Institute, 2002
- The effects of Al particle size on the burning rate and residual oxide in aluminized propellantsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2001
- The Details of Combustion of Ammonium Perchlorate Propellants: Leading Edge Flame DetachmentCombustion Science and Technology, 1998
- Comparison of Thermal Behavior of Regular and Ultra-fine Aluminum Powders (Alex) Made from Plasma Explosion ProcessCombustion Science and Technology, 1998
- Pressure dependence of burning rate of ammonium perchlorate-hydrocarbon binder solid propellantsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1997