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Design criteria for film cooling for small liquid-propellant rocket engines.

1969/02/01 by R. CARL STECHMAN, R. STECHMAN, JOELEE OBERSTONE +1
Engineering · #Rocket and propulsion systems research #Spacecraft and Cryogenic Technologies #Heat transfer and supercritical fluids

paper · doi:10.2514/3.29545

Abstract

Covers advancements in spacecraft and tactical and strategic missile systems, including subsystem design and application, mission design and analysis, materials and structures, developments in space sciences, space processing and manufacturing, space operations, and applications of space technologies to other fields.

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