The application of heat pipe technology to the design of rocket engine thrust chambers is discussed. Subjects presented are: (1) evaporator wick development, (2) specific heat pipe designs and test results, (3) injector design, fabrication, and cold flow testing, and (4) preliminary thrust chamber design. (Author)
Heat Pipe Technology for Advanced Rocket Thrust Chambers
1971
224 pages
Report
No indication
English
Heat pipe technology for advanced rocket thrust chambers
NTRS | 1971
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