Thermal reactivity of double-base rocket propellants

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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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.

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Deposited On:05 Jul 2011 10:46
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