Modeling Composite Solid Propellant with Catalytic Additives-Reference-Cited by-同舟云学术

Modeling Composite Solid Propellant with Catalytic Additives

Published:2013-01-05 Issue: Volume: Page:
ISSN:
Container-title:51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
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Author:

Frazier Corey¹,Demko Andrew¹,Petersen Eric¹

Affiliation:

1. Texas A&M University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2013-820

Reference18 articles.

1. A model of composite solid-propellant combustion based on multiple flames

2. 2Kreitz, K. R. "Catalytic Nanoparticle Additives in the Combustion of AP/HTPB Composite Solid Propellant," MS Thesis, Mechanical Engineering Department,Texas A&MUniversity,CollegeStation, TX,2010.

3. 3Kreitz, K. R., Petersen, E. L., Reid, D. L., and Seal, S. "Relative Dispersion of Catalytic Nanoparticle Additives and AP Particles inCompositeSolidPropellant andtheEffect onBurning Rate," AIAAPaper2011-418,Jan.2011.

4. Nanoscale Additives Tailor Energetic Materials

5. Multi-Parameter Study of Nanoscale TiO2 and CeO2 Additives in Composite AP/HTPB Solid Propellants

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