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.Full text not available from this repository. (Request a copy)
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|
|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|
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