Combustion response of ammonium perchlorate
Abstract
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.
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.Attached Files
Published - 401_Shusser_M_2000.pdf
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Additional details
- Eprint ID
- 20800
- Resolver ID
- CaltechAUTHORS:20101115-101901737
- California Institute of Technology
- Office of Naval Research Multidisciplinary Research Initiative
- N00014-95-I-1338
- Created
-
2010-11-29Created from EPrint's datestamp field
- Updated
-
2019-10-03Created from EPrint's last_modified field
- Caltech groups
- Guggenheim Jet Propulsion Center, GALCIT
- Series Name
- AIAA Papers
- Series Volume or Issue Number
- AIAA-2000-3694
- Other Numbering System Name
- AIAA
- Other Numbering System Identifier
- 2000-3694