Hybrid rocket propulsion systems have inherent safety and operational features that make them attractive choices for a broad range of applications including primary propulsion for launch vehicles, upper stage propulsion, tactical and strategic missile systems, and commercial space transportation. In Fundamentals of Hybrid Rocket Combustion and Propulsion the editors have gathered some of the most respected minds in the field to create a reference text designed for industrial designers, propulsion system analysts, test engineers, academic researchers, and graduate/undergraduate students studying chemical propulsion. The contents are organized to cover broad aspects of hybrid rocket combustion, including: theoretical and experimental approaches to solid-fuel regression rate characterization, both analytical and numerical modeling of hybrid rocket internal flow fields, transient hybrid combustion phenomena, various fuels and oxidizers used in hybrid rocket combustion, scaling effects relevant to hybrid motors, practical applications, and challenges for continued advancements in the hybrid rocket field. It is a useful springboard for future research and development efforts by industrial, government, and academic scientists and engineers so that the outstanding features of hybrid rockets will be fully realized.
Vortex Injection Hybrid Rockets
2007-01-01
30 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
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