Radiant Heating Tests of Several Liquid-Metal Heat-Pipe Sandwich Panels
Abstract
Integral heat-pipe sandwich panels, which synergistically combine the thermal efficiency of heat pipes and the structural efficiency of honeycomb sandwich construction, were conceived as a means of alleviating thermal stress problems in the Langley Scramjet Engine. Test panels which utilized two different wickable honeycomb cores, facesheets with screen mesh sintered to the internal surfaces, and a liquid metal working fluid (either sodium or potassium) were tested by radiant heating at various heat-load levels. The heat-pipe panels reduced maximum temperature differences by 31 percent with sodium working fluid and 45 percent with potassium working fluid. Results indicate that a heat-pipe sandwich panel is a potential, simple solution to the engine thermal stress problem. Other interesting applications of the concept include: cold plates for electronic component and circuit card cooling, radiators for large space platforms, low-distortion large area structures (e.g., space antennas) and laser mirrors.
- Publication:
-
Journal of Spacecraft and Rockets
- Pub Date:
- January 1984
- DOI:
- 10.2514/3.8598
- Bibcode:
- 1984JSpRo..21....4C
- Keywords:
-
- Engine Coolants;
- Engine Design;
- Engine Tests;
- Heat Pipes;
- Liquid Metals;
- Radiant Heating;
- Sandwich Structures;
- Supersonic Combustion Ramjet Engines;
- Cooling Systems;
- Engine Parts;
- Honeycomb Cores;
- Panels;
- Spacecraft Radiators;
- Thermal Stresses;
- Fluid Mechanics and Heat Transfer