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pro vyhledávání: '"Bulcher, A. Marc"'
Publikováno v:
Small Satellite Conference
Conventional hybrid rocket motors with thrust levels greater than 5 N rely on forced convection within the boundary layer as the primary heat-transfer mechanism for fuel vaporization. For hybrid rockets with thrust levels less than 5 N, oxidizer mass
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______1459::78d53229027042a7d9892009bde0f3f8
https://digitalcommons.usu.edu/smallsat/2020/all2020/157
https://digitalcommons.usu.edu/smallsat/2020/all2020/157
