This paper deals with air-hydrogen heat exchangers intended to provide in-flight oxygen collection capability to a reusable or semireusable two-stages-to-orbit launcher with an oxygen collection phase in supersonic cruise at Mach 2.5. It aims to present a theoretical but mainly technological and exp...
Highlights, strengths & weaknesses, commercial applications, and societal impact — written for this paper on demand.
No comments yet
Be the first to share your thoughts!