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Thermal Reactivity of Double-Base Rocket Propellants

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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