High Temperature Radiators for Electric Propulsion Systems
National Aeronautics and Space Administration
Agency Tracking Number:
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Small Business Information
Advanced Cooling Technologies, Inc.
1046 New Holland Ave., Lancaster, PA, 17601-5606
Socially and Economically Disadvantaged:
AbstractThe VASIMR propulsion system uses a high temperature Loop Heat Pipe (LHP) radiator to reject heat from the helicon section. The current baseline radiator uses titanium/water LHPs, however, deployable radiator and trace heating features are required to keep the water in the condenser from freezing when the radiator is turned off. The proposed project will develop high temperature toluene LHP radiators that will minimize the freezing problem, since the freezing temperature of toluene is roughly 100<SUP>o</SUP>C lower than water. Preliminary calculations on the toluene LHP radiator showed that a graded wick is required, with the pore size decreasing from the center to the surface of the wick. One goal of the project is to develop a graded alumina wick that reduces wick mass, back conduction, and pressure drop, enabling toluene as the working fluid. The ceramic wicks will also have near net shape fabrication, eliminating much of the current machining which adds costs to the LHP wicks. Optimizing the radial variation in porosity and permeability reduces the transport line sizes of toluene LHPs, significantly improving their mass and performance. The ceramic wicks can also be used in conventional LHPs, potentially reducing the LHP wick mass, pressure drop, and back conduction by 50 to 90% when compared with conventional nickel wicks. Phase I will demonstrate the feasibility of fabricating these wicks, demonstrate the wicks' machine-ability, conduct life tests, and evaluate the benefits of a graded wick versus a conventional wick with uniform properties. In Phase II, ACT will fabricate and test toluene LHP radiators with graded ceramic wicks to fully demonstrate their performances. We expect the technology to reach TRL 6 at the end of Phase II.
* information listed above is at the time of submission.