## 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 °C–170 °C) decomposition seems to involve diffusion controlled process, the
Artificial ageing of double base rocket propellant
✍ Scribed by S. Matečić Mušanić; M. Sućeska
- Book ID
- 106446174
- Publisher
- Springer Netherlands
- Year
- 2009
- Tongue
- English
- Weight
- 337 KB
- Volume
- 96
- Category
- Article
- ISSN
- 0022-5215
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