Loop Heat Pipe with Thermal Control Valve for Passive Variable Thermal Link

Award Information
Agency:
National Aeronautics and Space Administration
Branch
n/a
Amount:
$599,995.00
Award Year:
2011
Program:
SBIR
Phase:
Phase II
Contract:
NNX11CB96C
Award Id:
n/a
Agency Tracking Number:
095787
Solicitation Year:
2009
Solicitation Topic Code:
S3.02
Solicitation Number:
n/a
Small Business Information
1046 New Holland Ave., Lancaster, PA, 17601-5606
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
126288336
Principal Investigator:
John Hartenstine
Principal Investigator
(717) 295-6061
john.hartenstine@1-ACT.com
Business Contact:
Jon Zuo
President
(717) 717-6058
jon.zuo@1-ACT.com
Research Institution:
Stub




Abstract
Future Lunar Landers and Rovers will require variable thermal links that can reject heat during daytime, and passively shut-off during lunar night. During the long lunar day, the thermal management system must remove the waste heat from the electronics and batteries keep them within the acceptable temperature limit. Since the heater power availability is restricted, a variable thermal link is therefore required to limit the amount of heat that is removed from the electronics and radiated to space during the long lunar night. Conventional Loop Heat Pipes (LHPs) can provide the required variable thermal conductance, but they consume electrical power to shut down the heat transfer. Our innovation adds a Thermal Control Valve (TCV) to the LHP, allowing it to passively shut off without consuming any electrical power. This is important since there is a severe penalty for electrical power consumption: supplying 1 W in a photovoltaic system requires roughly 5 kg of extra equipment. The TCV used in the LHP has been previously selected for thermal control in the pumped loop on the Mars Science Laboratory. The Phase I project was successful in demonstrating the feasibility of integrating the TCV in a LHP. The Phase II project will fabricate and test a LHP with a TCV at representative conditions, bringing the technology to TRL 6. The testing will include full characterization of the TCV under various LHP operation modes. Analysis and testing of different LHP condenser layouts will also be performed, as well as freeze/thaw analysis.

* information listed above is at the time of submission.

Agency Micro-sites


SBA logo

Department of Agriculture logo

Department of Commerce logo

Department of Defense logo

Department of Education logo

Department of Energy logo

Department of Health and Human Services logo

Department of Homeland Security logo

Department of Transportation logo

Enviromental Protection Agency logo

National Aeronautics and Space Administration logo

National Science Foundation logo
US Flag An Official Website of the United States Government