Thermal Management System for Long-Lived Venus Landers

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: NNX10CC98P
Agency Tracking Number: 095939
Amount: $99,985.00
Phase: Phase I
Program: SBIR
Solicitation Topic Code: S3.03
Solicitation Number: N/A
Timeline
Solicitation Year: 2009
Award Year: 2010
Award Start Date (Proposal Award Date): 2010-01-29
Award End Date (Contract End Date): 2010-07-29
Small Business Information
1046 New Holland Avenue, Lancaster, PA, 17601-5688
DUNS: 126288336
HUBZone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: N
Principal Investigator
 Calin Tarau
 Principal Investigator
 (717) 295-6061
 calin.tarau@1-ACT.com
Business Contact
 Jon Zuo
Title: President
Phone: (717) 295-6058
Email: jonzuo@voicenet.com
Research Institution
N/A
Abstract
Long-lived Venus landers require power and cooling. Heat from the roughly 64 General Purpose Heat Source (GPHS) modules must be delivered to the convertor with minimal ÄT. The cooling system must be shutoff during the transit to Venus without overheating the GPHS modules. This program will develop an alkali metal Variable Conductance Heat Pipe (VCHP) integrated with a two-phase heat collection/transport package (HTP) between the GPHS stack and the convertor. The VCHP allows the Stirling converter to be shutoff during transit to Venus. The two-phase HTP minimizes the temperature drop between the multi-GPHS stack and the heater head. The HTP is required due to the large number of modules that must be interfaced, and the low allowable ÄT between the heater head temperature of 1200oC and the maximum allowable iridium cladding temperature in the GPHS (1266oC). The HTP also improves the convertor efficiency by decreasing the temperature non-uniformities at the high heat flux interface of the hot end of the heater head. It is superior to pumped liquid systems for transferring heat, because it eliminates the low efficiency liquid metal pump that they require. Other advantages of the system include low mass and volume, and a high degree of redundancy.

* 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
Environmental Protection Agency logo
National Aeronautics and Space Administration logo
National Science Foundation logo
US Flag An Official Website of the United States Government