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Development study of Hybrid Rocket Booster for Ballistic Lounch of Small Satellite
小型衛星のためのハイブリッドロケットの打ち上げ機の開発
International journal of microgravity science and application
小型衛星のためのハイブリッドロケットの打ち上げ機の開発
Preserved Fulltext
For the use of ballistic launches of a small satellite, the development study of a high thrust hybrid rocket motor has been made. To enhance the regression rate of the solid fuel and augment the thrust, the authors employed a new fuel conˆguration. This new conˆguration allows mixing and combustion to occur around the stagnation points on solid fuel surfaces. The static ˆring tests using a LOX/PMMA hybrid motor with a LOX cooling system have proved su‹ciently prompt ignition, high thrust level,
doi:10.15011/jasma.19.2.112
fatcat:vmdk24x5fzexhg3dktna2jk5ey