## 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
Platonization in double-base rocket propellants
β Scribed by SINGH, H.; RAO, K. R. K.
- Book ID
- 120379341
- Publisher
- American Institute of Aeronautics and Astronautics
- Year
- 1977
- Tongue
- English
- Weight
- 778 KB
- Volume
- 15
- Category
- Article
- ISSN
- 0001-1452
- DOI
- 10.2514/3.7457
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## Abstract In a continuous joint research program, the Department of Aerospace Engineering of DUT and the Technological Laboratory TNO investigate unstable combustion of solid rocket propellants. Some results of this research program are discussed here. The oscillatory combustion phenomenon is dis