Please use this identifier to cite or link to this item:
http://nopr.niscpr.res.in/handle/123456789/29974Full metadata record
| DC Field | Value | Language |
|---|---|---|
| dc.contributor.author | Venugopalan, S | - |
| dc.contributor.author | Sarwade, D B | - |
| dc.contributor.author | Agrawal, J P | - |
| dc.date.accessioned | 2014-11-13T09:16:57Z | - |
| dc.date.available | 2014-11-13T09:16:57Z | - |
| dc.date.issued | 1994-10 | - |
| dc.identifier.issn | 0975-1017 (Online); 0971-4588 (Print) | - |
| dc.identifier.uri | http://hdl.handle.net/123456789/29974 | - |
| dc.description | 289-291 | en_US |
| dc.description.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. | en_US |
| dc.language.iso | en_US | en_US |
| dc.publisher | NISCAIR-CSIR, India | en_US |
| dc.rights |  CC Attribution-Noncommercial-No Derivative Works 2.5 India | en_US |
| dc.source | IJEMS Vol.01(5) [October 1994] | en_US |
| dc.title | Role of oxygen balance on the thermal decomposition behaviour of composite propellants | en_US |
| dc.type | Article | en_US |
| 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 |
Items in NOPR are protected by copyright, with all rights reserved, unless otherwise indicated.