NASA STTR 2018-I Solicitation

Proposal Summary


PROPOSAL NUMBER:
 18-1- T9.01-8702
SUBTOPIC TITLE:
 Lander Systems Technology
PROPOSAL TITLE:
 Advanced Hot Reservoir Variable Conductance Heat Pipes for Planetary Landers
SMALL BUSINESS CONCERN (SBC):
RESEARCH INSTITUTION (RI):
Name:   Advanced Cooling Technologies, Inc.
Name:   Case Western Reserve University
Street:  1046 New Holland Avenue
Street:  10900 Euclid Ave.
City:   Lancaster
City:   Cleveland
State/Zip:  PA  17601-5688
State/Zip:   OH 44106
Phone:  (717) 205-0602
Phone:   (216) 368-6455


Principal Investigator (Name, E-mail, Mail Address, City/State/Zip, Phone)
Dr. Kuan-Lin Lee
kuan-lin.lee@1-act.com
1046 New Holland Avenue Lancaster, PA 17601 - 5688
(717) 205-0631

Business Official (Name, E-mail, Mail Address, City/State/Zip, Phone)
Dr. William Anderson
Bill.Anderson@1-act.com
1046 New Holland Avenue Lancaster, PA 17601 - 5688
(717) 205-0602
Estimated Technology Readiness Level (TRL) :
Begin: 4
End: 5
Technical 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.

Potential NASA Applications

The next generation of polar rovers and equatorial landers is the immediate NASA application. A hot reservoir VCHP with enhanced reliability will be needed, which is able to operate during large tilts, shut down during the long Lunar night and maintain the temperature lander vehicle over a wide sink temperature fluctuation on the Lunar surface.

Potential Non-NASA Applications

Astrobotics Technology, as one of the primary developers of space robotics for planetary missions has expressed a great interest on ACT’s hot reservoir VCHP technology and anticipate to apply the advanced version to their lander vehicles for Lunar and Mars surface operation.


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