Christoph Bauer, Reinhold Baumann, Guido Kurth, Ralf Schlaps , Johan Steelant and Philipp
Störchle

DOI Number XXX-YYY-ZZZ

Conference Number HiSST-2022-304

SABRE – Synergetic Air Breathing Rocket Engine – combines the advantages of a high specific impulse
air breathing engine with a high thrust/weight ratio rocket motor. During air breathing mode, SABRE –
operating in a combined turbomachinery based cycle of the core engine and ramjet cycle of the bypass
burner – captures the ambient air as oxidizer [1]. To minimize drag, the adjustable air intake system is
capable of aligning the shock structure to the free stream Mach number and capturing the maximum
possible air mass flow.

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In Categories: 1.Events, HiSST 2022, Propulsion Systems and Components
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