Assessing the Mixedness of Composite Solid Rocket Propellants Using Fluorescent Particles
Author:
Affiliation:
1. Texas A&M University, College Station, Texas 77843
2. University of Central Florida, Orlando, Florida 32816
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.40984
Reference14 articles.
1. High-Pressure Testing of Composite Solid Propellant Mixtures: Burner Facility Characterization
2. Multi-Parameter Study of Nanoscale TiO2 and CeO2 Additives in Composite AP/HTPB Solid Propellants
3. Role of the Scanning Electron Microscope in the Study of Solid Rocket Propel I ant Combustion, I. Ammonium Perchlorate Decomposition and Deflagration
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