The combustion of composite solid propellants was studied using ammonium dichromate, chromium carbonate, chromium oxide, basic copper carbonate and cupric oxide as additives. Burning rates were considerably enhanced in each case. Flame temperatures were measured and found to be higher than in cases
Burn Rate Models for Gun Propellants
✍ Scribed by Norbert Eisenreich; Thomas S. Fischer; Gesa Langer; Stefan Kelzenberg; Volker Weiser
- Publisher
- John Wiley and Sons
- Year
- 2002
- Tongue
- English
- Weight
- 237 KB
- Volume
- 27
- Category
- Article
- ISSN
- 0721-3115
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