Shusser, Michael and Culick, Fred E. C. and Cohen, Norman S. (2000) Combustion response of ammonium perchlorate. AIAA Papers, AIAA-2000-3694. American Institute of Aeronautics and Astronautics . http://resolver.caltech.edu/CaltechAUTHORS:20101115-101901737
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A modified Price-Boggs-Derr model is applied to compute the linear and non-linear combustion response properties of monopropellant ammonium perchlorate. The kinetics constants were changed to achieve good agreement with response function data as well as with steady-state data. The numerical method was first validated by comparing computations using the Levine & Culick boundary condition in the limit of small perturbations with the exact mathematical solution for linear response. Then, using the AP model for the boundary condition, various linear and non-linear computations were performed. Supplemental mathematical analyses relate the AP model to the basic two parameters of the classical theory and show the key factors determining the nature of the combustion response.
|Item Type:||Report or Paper (Report)|
|Additional Information:||© 2000 The American Institute of Aeronautics and Astronautics Inc. This work is sponsored partly by the California Institute of Technology and partly by the Office of Naval Research Multidisciplinary University Research Initiative under grant No. N00014-95-I-1338. Dr. Judah Goldwasser is the Navy Program Manager.|
|Group:||Guggenheim Jet Propulsion Center|
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|Official Citation:||Combustion response of ammonium perchlorate Shusser, Michael, California Inst. of Technology, Pasadena; Culick, Fred E. C., California Inst. of Technology, Pasadena; Cohen, Norman S., Cohen Professional Services, Redlands, CA AIAA-2000-3694 AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 36th, Huntsville, AL, July 16-19, 2000|
|Usage Policy:||No commercial reproduction, distribution, display or performance rights in this work are provided.|
|Deposited By:||Ruth Sustaita|
|Deposited On:||29 Nov 2010 19:00|
|Last Modified:||26 Dec 2012 12:38|
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