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Advanced Hot Reservoir Variable Conductance Heat Pipes for Planetary Landers

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: 80NSSC18P2155
Agency Tracking Number: 188702
Amount: $124,997.00
Phase: Phase I
Program: STTR
Solicitation Topic Code: T9
Solicitation Number: STTR_18_P1
Timeline
Solicitation Year: 2018
Award Year: 2018
Award Start Date (Proposal Award Date): 2018-07-27
Award End Date (Contract End Date): 2019-08-26
Small Business Information
1046 New Holland Avenue
Lancaster, PA 17601-5688
United States
DUNS: 126288336
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
Principal Investigator
 Kuan-Lin Lee
 (717) 205-0631
 kuan-lin.lee@1-act.com
Business Contact
 Franklin Morales
Phone: (717) 205-0637
Email: frank.morales@1-act.com
Research Institution
 Case Western Reserve University
 
10900 Euclid Ave.
Cleveland, OH 44106-0000
United States

 Federally Funded R&D Center (FFRDC)
Abstract

In contrast to the standard cold reservoir Variable Conductance Heat Pipe (VCHP) where for tight thermal control an electrical heater is used for the reservoir (wicked), Advanced Cooling Technologies, Inc (ACT) developed a hot reservoir VCHP with the reservoir thermally coupled to the evaporator. This novel feature will provide a tight temperature control capability without the need for control power. Based on the recent ISS testing result, it was concluded that working fluid management within the reservoir and the NCG tube (typically non-wicked) of VCHPs is the key to advance the reliability of a hot reservoir VCHP, which will secure a successful long-term mission of planetary landers. Under this STTR topic, ACT will collaborate with Case Western Reserve University (CWRU) to implement several novel fluid management features to enhance system reliability of hot reservoir VCHP. ACT will develop several advanced fluid management features and test their performance on a hot reservoir VCHP prototype. In parallel, CWRU will perform a fundamental study and mathematical model development to simulate and understand the complexity of the transport phenomena problem within the two-phase working fluid and non-condensable gas mixture in the reservoir and the NCG tube. The objective of the CWRU’s effort is to bring deep understanding of the thermal-fluid and thermodynamic environment in the VCHP reservoir and NCG tube and identify an effective purging mechanism (i.e. vapor removal from a hot reservoir), which is crucial in designing a reliable hot reservoir VCHP for future planetary lander thermal management.

* Information listed above is at the time of submission. *

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