The hydroxy-terminated polybutadiene (HTPB) based composite propellants without any metal additive and with varying concentration of metal additives such as iron oxide, copperchromite, strontium carbonate and lithium fluoride have been cast and cured. These propellants have been characterized for de
β¦ LIBER β¦
Effect of Binders on the Burning Rate of AP Composite Propellants
β Scribed by Hakobu Bazaki; Naminosuke Kubota
- Publisher
- John Wiley and Sons
- Year
- 2000
- Tongue
- English
- Weight
- 127 KB
- Volume
- 25
- Category
- Article
- ISSN
- 0721-3115
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