Ramaprasad, P. R. ; Raghunandan, B. N. ; Mukunda, H. S. (1983) Some experiments on model composite solid propellants Propellants, Explosives, Pyrotechnics, 8 (2). pp. 53-55. ISSN 0721-3115
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Official URL: http://onlinelibrary.wiley.com/doi/10.1002/prep.19...
Related URL: http://dx.doi.org/10.1002/prep.19830080206
Abstract
Experiments on two-dimensional model propellants using cylindrical oxidizer (ammonium perchlorate) pellets in a fuel matrix (CTPB) are described. Measurements show that burning rate of AP in the fuel environment is lower than of pure AP. The oxidizer-to-fuel ratio seems to be fuel-rich when the oxidizer particles are imbedded in contact with the fuel and it becomes oxidizer-rich for a non-zero separation between oxidizer particle and the fuel.
| Item Type: | Article |
|---|---|
| Source: | Copyright of this article belongs to John Wiley and Sons, Inc. |
| ID Code: | 23205 |
| Deposited On: | 25 Nov 2010 13:19 |
| Last Modified: | 08 Jun 2011 06:26 |
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