Honeycomb panel heat pipe development for space radiatorsAn assessment of the honeycomb panel heat pipe concept as a moderate temperature range, low-mass, highly efficient radiator fin for the NASA Space Station is presented, based on test results for a thin-wall (0.46 mm) all-welded stainless steel sample with core depth of 63.5 mm and a hexagonal-cell size of 127.7 mm. The 0.61 x 3.05 m test segment, operating with methanol as a working fluid, exhibited a maximum heat transfer rate of 600 W at 50 C and was isothermal to within + or - 2 C almost entirely throughout the surface. Tilt testing, which comprised relocation of the heater along one edge of the panel, resulted in maximum power levels of 70 and 50 W at panel elevations of 12.7 and 25.4 mm, respectively. As-designed panel performance is predicted to be from 500 to 1000 W over the range of operating temperatures; better performance is predicted for an open-channel design.
Document ID
19850055477
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Tanzer, H. J. (Hughes Aircraft Co. Torrance, CA, United States)
Fleischman, G. L. (Hughes Aircraft Co. Torrance, CA, United States)
Rankin, J. G. (NASA Johnson Space Center Houston, TX, United States)
Date Acquired
August 12, 2013
Publication Date
June 1, 1985
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 85-0978Report Number: AIAA PAPER 85-0978