NASA SBIR 2018-II Solicitation

Proposal Summary

 18-2- Z2.01-4863
 Thermal Management
 Thermochromics with Very Low Transition Temperature
SMALL BUSINESS CONCERN (Firm Name, Mail Address, City/State/Zip, Phone)
Triton Systems, Inc.
200 Turnpike Road
Chelmsford, MA 01824
(978) 250-4200

PRINCIPAL INVESTIGATOR (Name, E-mail, Mail Address, City/State/Zip, Phone)
Lawrence Domash
200 Turnpike Road
Chelmsford, MA 01824 - 4040
(617) 645-8456

BUSINESS OFFICIAL (Name, E-mail, Mail Address, City/State/Zip, Phone)
Collette Jolliffe
200 Turnpike Road
Chelmsford, MA 01824 - 4040
(978) 856-4158

Estimated Technology Readiness Level (TRL) :
Begin: 2
End: 4
Technical Abstract (Limit 2000 characters, approximately 200 words)

Triton Systems is developing an unpowered thermostatic film for application to spacecraft surfaces. We call our approach Phase Change Thermochromic Radiator (PCTR); it self-switches from low to high emittance above a designed temperature setpoint Tc, causing a surface in space to radiate heat only when it becomes too warm and conserving heat otherwise. Key to the operation of PCTR is a phase change material integrated into a multilayer thin film structure to produce a device which is reflective over the 3-35 µm IR band below a transition temperature Tc but strongly absorptive above Tc. PCTR has advantages over competing approaches to dynamic emissivity in that it requires no electrical drive power, is relatively simple to fabricate, and contains only stable and rugged materials. Phase I research showed a path to significantly reduce the operational transition temperature, with 5°C or below being the ultimate goal of the program. In Phase II, complete devices will be demonstrated with turndown ratio of at least 6:1 and potentially 10:1. Scalable fabrication methods will be developed. Key qualification tests will include thermal cycling, vibration, peel tests, surface charge and degradation over operational life.

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

PCTR is applicable to a variety of NASA missions from nanosatellites in LEO to large manned vehicles on interplanetary missions. The design can be customized for a Tc and emissivity to match the mission. Higher temperature versions may be used for propulsion systems.

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

PCTR thermostatic films may have applications to military and communications satellites, and otherwise in commercial applications in the architecture market for thermal management of buildings



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