NASA SBIR 2018-I Solicitation

Proposal Summary


PROPOSAL NUMBER:
 18-1- Z2.01-8692
SUBTOPIC TITLE:
 Thermal Management
PROPOSAL TITLE:
 Consumable-Based Cooling for 24 Hour Life Venus Lander
SMALL BUSINESS CONCERN (Firm Name, Mail Address, City/State/Zip, Phone)
Advanced Cooling Technologies, Inc.
1046 New Holland Avenue
Lancaster , PA 17601-5688
(717) 205-0602

Principal Investigator (Name, E-mail, Mail Address, City/State/Zip, Phone)
Dr. Calin Tarau
calin.tarau@1-act.com
1046 New Holland Avenue Lancaster, PA 17601 - 5688
(717) 205-0659

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: 2
End: 4
Technical Abstract

A reliable thermal management system that will enable at least 24-hours survival of Venus landers in the extreme environment (460°C, 92 bar) is highly desirable for NASA future Venus in-situ exploration missions. In response to the NASA SBIR solicitation, Advanced Cooling Technologies, Inc. (ACT) proposes to develop a consumable-based cooling system for Venus landers waste heat rejection. The proposed system consists of two pressurized vessels: a primary vessel charged with a consumable fluid in a saturation state (ammonia) and a secondary vessel filled with compressed gas. The main role of the compressed gas is to help ammonia vapor venting into a higher-pressure environment than the vapor pressure that corresponds to the cooled electronics temperature. Through venting a mixture of consumable vapor and compressed gas to the Venus ambient, a significant amount of evaporative cooling (primary) and Joule-Thompson cooling (secondary) can be achieved, which not only will keep the electronics temperature cool but also provide heat guarding by collecting and removing the incoming heat leaks from Venus environment. In Phase I, a proof-of-concept consumable based prototype will be fabricated and tested. Test results will be used to validate a mathematical model. After validation, the model will be employed to design the full-scale prototype and optimize mass and thermal performance. A preliminary modeling result shows a thermal management system total mass (fluids and structure) of 75kg.

Potential NASA Applications

The proposed consumable-based cooling system represents a passive, low-mass and effective thermal management solution that will enable a Venus lander to survive and operate for more than 24 hours in the extreme environment, making the future Venus “human-in-the-loop” mission durable. The innovative thermal management technology will be beneficial to several planned Venus in-situ exploration missions such as Flagship and New Frontiers missions.

Potential Non-NASA Applications

The consumable-based cooling technology can be applied to thermal management systems in high pressure environments, such as small-scale unmanned undersea vehicles (UUV) or submarines.  It can also be used to cool military electronics by vapor venting.


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