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http://nopr.niscpr.res.in/handle/123456789/29974| Title: | Role of oxygen balance on the thermal decomposition behaviour of composite propellants |
| Authors: | Venugopalan, S Sarwade, D B Agrawal, J P |
| Issue Date: | Oct-1994 |
| Publisher: | NISCAIR-CSIR, India |
| Abstract: | Differential thermal analysis (DTA) on amonium perchlorate (AP), hydroxy terminated polybutadiene (HTPB) based polyurethane (PO) and other composite propellant compositions consisting of AP and PO matrix has been studied. The data show that as the oxygen balance (OB) of the propellant composition decreases the decomposition rate of AP during the second stage (deflagration exotherm-Exo II) around 360ᵒ C rises very significantly due to the increase in calorific values. |
| Page(s): | 289-291 |
| ISSN: | 0975-1017 (Online); 0971-4588 (Print) |
| Appears in Collections: | IJEMS Vol.01(5) [October 1994] |
Files in This Item:
| File | Description | Size | Format | |
|---|---|---|---|---|
| IJEMS 1(5) 289-291.pdf | 253 kB | Adobe PDF | View/Open |
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