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Thermal Reactivity of Double-Base Rocket Propellants

✍ Scribed by V. R. Pai Verneker; K. Kishore; C. B. V. Subhas

Publisher
John Wiley and Sons
Year
1979
Tongue
English
Weight
345 KB
Volume
4
Category
Article
ISSN
0721-3115

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✦ Synopsis

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 Β°C–170 Β°C) decomposition seems to involve diffusion controlled process, the mechanism in air and vacuum being different. High temperature (170 °–205 Β°C) decomposition involves bond breakage.

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