While burning at subatmospheric pressure, composite propellants generally fume and under certain conditions eject partially reacted particles. This characteristic property is exploited in this study to understand the mechanism of burning rate modification. The additives CuCr204, Fe203, Sb2 03, AI(OH
Role of Boron in Burning Rate Augmentation of AP composite propellants
โ Scribed by T. Kuwahara; N. Kubota
- Publisher
- John Wiley and Sons
- Year
- 1989
- Tongue
- English
- Weight
- 357 KB
- Volume
- 14
- Category
- Article
- ISSN
- 0721-3115
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