Published July 2000 | Version Published
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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.

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Identifiers

Eprint ID
20800
Resolver ID
CaltechAUTHORS:20101115-101901737

Funding

California Institute of Technology
Office of Naval Research Multidisciplinary Research Initiative
N00014-95-I-1338

Dates

Created
2010-11-29
Created from EPrint's datestamp field
Updated
2019-10-03
Created from EPrint's last_modified field

Caltech Custom Metadata

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