Thermal Reactivity of Double-Base Rocket
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V. R. Pai Verneker; K. Kishore; C. B. V. Subhas
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Article
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1979
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John Wiley and Sons
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English
β 345 KB
## Abstract Thermal decomposition studies on doubleβbase propellants have been carried out in air and vacuum using differential scanning calorimetric, thermogravimetric and mass spectrometric techniques. Low temperature (90 Β°Cβ170 Β°C) decomposition seems to involve diffusion controlled process, the