This paper examines the effect of single protrusion and multiprotrusion on the performance of hybrid rocket with the length/initial port diameter (L/D) ratio of 12.5. The fuel used was wax,… Click to show full abstract
This paper examines the effect of single protrusion and multiprotrusion on the performance of hybrid rocket with the length/initial port diameter (L/D) ratio of 12.5. The fuel used was wax, and the...
               
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