Verneker, Pai VR and Kishore, K and Subhas, CBV (1979) Thermal Reactivity of Double-Base Rocket Propellants. In: Propellants, Explosives, Pyrotechnics, 4 (4). pp. 83-86.
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Thermal decomposition studies on double-base propellants have been carried out in air and vacuum using differential scanning calorimetric, thermogravimetric and mass spectrometric techniques. Low temperature (90 degree C-170 degree C) decomposition seems to involve diffusion controlled process, the mechanism in air and vacuum being different. High temperature (170 degree -205 degree C) decomposition involves bond breakage.
| Item Type: | Journal Article |
|---|---|
| Publication: | Propellants, Explosives, Pyrotechnics |
| Publisher: | Verlag GmbH & Co. KGaA, Weinheim |
| Additional Information: | The copyright belongs to Verlag GmbH & Co. KGaA, Weinheim. |
| Department/Centre: | Division of Chemical Sciences > Inorganic & Physical Chemistry |
| Date Deposited: | 03 Nov 2005 |
| Last Modified: | 27 Aug 2008 11:32 |
| URI: | http://eprints.iisc.ac.in/id/eprint/3925 |
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