An improvement in the performance of solid rocket motors was achieved by increasing the oxidizer content of HTPB-based solid propellants. To minimize the adverse changes in the mechanical and rheological properties due to the increased amount of hard solid particles in the soft polymeric binder matr
β¦ LIBER β¦
Mechanical Properties of Plateau Burn Azide Composite Propellants
β Scribed by Yoshio Oyumi
- Publisher
- John Wiley and Sons
- Year
- 1999
- Tongue
- English
- Weight
- 201 KB
- Volume
- 24
- Category
- Article
- ISSN
- 0721-3115
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