NASA NTRS · 19730022965
Liquid rocket engine fluid-cooled combustion chambers
Abstract
A monograph on the design and development of fluid cooled combustion chambers for liquid propellant rocket engines is presented. The subjects discussed are (1) regenerative cooling, (2) transpiration cooling, (3) film cooling, (4) structural analysis, (5) chamber reinforcement, and (6) operational problems.
Keep this discovery
Explore connections, maps & timelines
1972-04-01. Liquid rocket engine fluid-cooled combustion chambers. https://ntrs.nasa.gov/citations/19730022965
Cite the original work for its findings. Save a collection to share your selection of sources.