Thermal Reactivity of Double‐Base Rocket Propellants

descriptionPublicationkeyboard_double_arrow_right Article 01 Aug 1979 India English Publisher:WileyJournal:Propellants, Explosives, Pyrotechnics, volume 4, pages 83-86 (issn: 0721-3115, eissn: 1521-4087,

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Authors: Verneker, Pai VR; Kishore, K; Subhas, CBV;

doi: 10.1002/prep.19790040406

Thermal Reactivity of Double‐Base Rocket Propellants

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Abstract

AbstractThermal 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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India

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Inorganic & Physical Chemistry

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