Integral heat-pipe sandwich panels, which synergistically combine the thermal efficiency of heat pipes and the structural efficiency of honeycomb sandwich panel construction, were fabricated and tested. The designs utilize two different wickable honeycomb cores, facesheets with screen mesh sintered to the internal surfaces, and potassium or sodium as the working fluid. Panels were tested by radiant heating, and the results indicate successful heat pipe operation at temperatures of approximately 922K (1200F). These panels, in addition to solving potential thermal stress problems in an Airframe-Integrated Scramjet Engine, have potential applications as cold plates for electronic component cooling, as radiators for space platforms, and as low...
The feasibility of fabricating and processing moderate temperature range heat pipes in a low mass ho...
Refractory-composite/heat-pipe-cooled wing an tail leading edges are being considered for use on hyp...
Heat-transfer has been performed on a sandwich thermal protection system (TPS) for future flight veh...
Integral heat pipe sandwich panels, which synergistically combine the thermal efficiency of heat pip...
The feasibility of fabricating and processing liquid metal heat pipes in a low mass honeycomb sandwi...
The feasibility of performance enhancing the sandwich panel heat pipe was investigated for moderate ...
The feasibility of fabricating and processing moderate temperature range vapor chamber type heat pip...
The results of a program to design and fabricate an unshielded actively cooled structural panel for ...
The panel assembly consisted of an external thermal protection system (metallic heat shields and ins...
Nonlinear mathematical programming methods are used to design a radiantly cooled and heat-pipe-coole...
The development, fabrication, and evaluation of heat pipe thermal conditioning panels are discussed....
The construction of two test modules is presented for a feasibility demonstration of a concept for r...
Stainless-steel honeycomb-core sandwich panels which differed primarily in skin thicknesses were tes...
Progress brought about by human ingenuity and technological developments has been always accompanied...
The status of the structural development of an integral cryogenic-tankage/hot-fuselage concept for f...
The feasibility of fabricating and processing moderate temperature range heat pipes in a low mass ho...
Refractory-composite/heat-pipe-cooled wing an tail leading edges are being considered for use on hyp...
Heat-transfer has been performed on a sandwich thermal protection system (TPS) for future flight veh...
Integral heat pipe sandwich panels, which synergistically combine the thermal efficiency of heat pip...
The feasibility of fabricating and processing liquid metal heat pipes in a low mass honeycomb sandwi...
The feasibility of performance enhancing the sandwich panel heat pipe was investigated for moderate ...
The feasibility of fabricating and processing moderate temperature range vapor chamber type heat pip...
The results of a program to design and fabricate an unshielded actively cooled structural panel for ...
The panel assembly consisted of an external thermal protection system (metallic heat shields and ins...
Nonlinear mathematical programming methods are used to design a radiantly cooled and heat-pipe-coole...
The development, fabrication, and evaluation of heat pipe thermal conditioning panels are discussed....
The construction of two test modules is presented for a feasibility demonstration of a concept for r...
Stainless-steel honeycomb-core sandwich panels which differed primarily in skin thicknesses were tes...
Progress brought about by human ingenuity and technological developments has been always accompanied...
The status of the structural development of an integral cryogenic-tankage/hot-fuselage concept for f...
The feasibility of fabricating and processing moderate temperature range heat pipes in a low mass ho...
Refractory-composite/heat-pipe-cooled wing an tail leading edges are being considered for use on hyp...
Heat-transfer has been performed on a sandwich thermal protection system (TPS) for future flight veh...