Closed-Form Equations to Evaluate Heat-Pipe-Cooled Leading-Edge Design Feasibility
David E. Glass
Journal of Spacecraft and Rockets ; 37 , 1 ; 147-150
2000-01-01
4 pages
Article (Journal)
Electronic Resource
English
Design, analysis, and tests of a shuttle-type heat-pipe-cooled leading edge
Tema Archive | 1979
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