A re-entrant groove hydrogen heat pipeThis paper extends the development of reentrant groove technology to hydrogen heat pipes. Parametric analyses are presented which optimize the theoretical design while considering the limitations of state-of-the-art extrusion technology. Acceptable production-type runs of extruded lengths (over 300 m) could only be achieved at the expense of a wider nominal groove opening than specified (0.33 mm vs. 0.20 mm). However, dimensional variations of other critical dimensions were within 0.05 mm, which exceeded expectations. The 6063-T6 aluminum extrusion is 14.6 mm OD with a wall thickness of 1.66 mm and contains 20 axial grooves which surround a central 9.3-mm-diam vapor core. Each axial groove is 0.775-mm-diam with a 0.33 mm opening. An excess vapor reservoir is provided at the evaporator to minimize the pressure containment hazard during ambient storage. Details of the instrumentation and helium-cooled test installation are also presented.
Document ID
19780051694
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Alario, J. (Grumman Aerospace Corp. Bethpage, NY, United States)
Kosson, R. (Grumman Aerospace Corp. Bethpage, N.Y., United States)
Mccreight, C. (NASA Ames Research Center Moffett Field, Calif., United States)