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.
Rocket nozzle coolant channel thermal analysis program (E25107)
14.04.1972
Report
Keine Angabe
Englisch
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