NASA SBIR 2022-I Solicitation

Proposal Summary

Proposal Information

Proposal Number:
22-1- Z2.01-1555
Subtopic Title:
Spacecraft Thermal Management
Proposal Title:
A Compact, Gravity-Insensitive Gas Trap for Extreme Temperature Environments

Small Business Concern

   
Firm:
          
Creare, LLC
          
   
Address:
          
16 Great Hollow Road, Hanover, NH 03755
          
   
Phone:
          
(603) 643-3800                                                                                                                                                                                
          

Principal Investigator:

   
Name:
          
Thomas Conboy
          
   
E-mail:
          
tmc@creare.com
          
   
Address:
          
16 Great Hollow Road, NH 03755 - 3116
          
   
Phone:
          
(603) 643-3800                                                                                                                                                                                
          

Business Official:

   
Name:
          
Patrick Magari
          
   
E-mail:
          
contractsmgr@creare.com
          
   
Address:
          
16 Great Hollow Road, NH 03755 - 3116
          
   
Phone:
          
(603) 643-3800                                                                                                                                                                                
          

Summary Details:

   
Estimated Technology Readiness Level (TRL) :                                                                                                                                                          
Begin: 3
End: 5
          
          
     
Technical Abstract (Limit 2000 characters, approximately 200 words):

NASA is actively working towards missions involving crewed habitats for extended stays on the lunar surface and other similar environments in space. Environmental control of these habitats is enabled by use of thermal control systems to maintain conditions within a tight band. These thermal control systems must be highly reliable, lightweight, and able to effectively control cabin and equipment temperatures to within several degrees under varying heat loads. In these systems, the pump is often the only dynamic component and thus poses the greatest risk of failure. To address this need, Creare has developed a compact, gravity-insensitive gas trap capable of passively sequestering, then venting non-condensable gas buildup in liquid coolant loops. The gas trap is fully welded with metallic wetted surfaces, can be regenerated to eliminate fouling, and is compatible with operation in extreme environments. In Phase I, we will prove the feasibility of this approach by developing a preliminary gas trap design, demonstrating key processes involved in fabrication of the gas trap including development of the superhydrophobic titanium porous tube, and characterizing a subscale gas trap through laboratory testing. In Phase II, we will fabricate a gas trap capable of serving a multi-kW spaceborne thermal coolant loop, demonstrate its performance in a representative thermal environment, and deliver it to NASA for further performance evaluation.

          
          
     
Potential NASA Applications (Limit 1500 characters, approximately 150 words):

Gas traps are needed for enhanced reliability in thermal control for NASA missions including on-board the ISS. The current proposed effort would enable high reliability coolant loops for use in future lunar habitats or extreme environments circulating low-surface-tension fluids. Other governmental applications (e.g., DoD) are similar to NASA uses, specifically high reliability coolant loops operating in extreme environments for aircraft, ships, and ground vehicles.

          
          
     
Potential Non-NASA Applications (Limit 1500 characters, approximately 150 words):

The superhydrophobic membrane development has commercial applications for various chemical industries including steam separation and chemical processing with two-phase caustic chemical flows. The gas trap itself has application in high reliability coolant with minimal available maintenance such as in nuclear power plants or in other remote power stations.

          
          
     
Duration:     6
          
          

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