Pai Verneker, V. R. ; Kishore, K. ; Subhas, C. B. V. (1979) Thermal reactivity of double-base rocket propellants Propellants, Explosives, Pyrotechnics, 4 (4). pp. 83-86. 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.19790040406
Abstract
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°C-170°C) decomposition seems to involve diffusion controlled process, the mechanism in air and vacuum being different. High temperature (170°–205°C) decomposition involves bond breakage.
Item Type: | Article |
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Source: | Copyright of this article belongs to John Wiley and Sons. |
ID Code: | 32187 |
Deposited On: | 05 Jul 2011 10:46 |
Last Modified: | 05 Jul 2011 10:46 |
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