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Abstract:
We apply our experimental and modeling results of a number of burner-stabilized flames relevant to the combustion of solid propellants to calculate the burning rates of tri-amino-guanidinium-azotetrazolate (TAGzT) with and without a nitrate ester-based propellant using our CYCLOPS combustion model that we developed at US Army Research Laboratory. The model employs a detailed, chemical reaction mechanism containing 59 species and 368 reactions. Our calculations show that TAGzT enhances the burning rate of the base propellant over a range of pressures used for rockets and guns; a factor of three at 10 MPa.
| Limitations: |
 APPROVED FOR PUBLIC RELEASE |
| Description: |
Conference paper |
| Pages: |
6 |
| Report Date: |
Dec 2008 |
| Report Number: |
A008505 |
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