NASA NTRS · 19730017105
Rocket nozzle coolant channel thermal analysis program (E25107)
Abstract
A complete description of the liquid cooled rocket nozzle analysis program (E25107) is presented, including a users manual, program listing, and a sample problem. The program is recommended for use in designing liquid cooled rocket nozzles. In addition, it is adaptable to any system in which a liquid-cooled tubular structure is used to contain and direct the flow of a hot gas.
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Thompson, W. R.. 1972-04-14. Rocket nozzle coolant channel thermal analysis program (E25107). https://ntrs.nasa.gov/citations/19730017105
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