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Site and Mode of Action of Platonizers in Double Base Propellants

✍ Scribed by KUBOTA, N.; OHLEMILLER, T.J.; CAVENY, L.H.; SUMMERFIELD, M.

Book ID
120379339
Publisher
American Institute of Aeronautics and Astronautics
Year
1974
Tongue
English
Weight
873 KB
Volume
12
Category
Article
ISSN
0001-1452

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## 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