Improved injector for oxygen difluoride and diborane has better mixing characteristics and is able to project fuel onto the wall of the combustion chamber for better cooling. It produces an essentially conical, diverging, continuous sheet of propellant mixture formed by similarly shaped and continuously impinging sheets of fuel and oxidant.
Single-element coaxial injector for rocket fuel
01.10.1969
Sonstige
Keine Angabe
Englisch
Cryogenic Flow and Mixing from a Single Element Coaxial Rocket Injector
British Library Conference Proceedings | 2006
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