SBIR/STTR Research Award

Flexible Variable Emission Material

Award identifier f62bfbf3c053f70c803c2389358e2d8f3c2d8f9ea04ee7f440fc27ef7c52126dAwarding agency National Aeronautics and Space Administration

Award amount

$849,444

Program and phase

SBIR · Phase II

Award year

2025

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
PLASMONICS INC
Proposal award date
2025-08-13
Contract end date
2027-08-17
UEI
ZCD2ULL43U14
Solicitation number
SBIR 2024-II
Topic code
S16

Research abstract

Thermal management is an enduring need for all space platforms and vehicles. Spacecraft are routinely exposed to extreme temperature fluctuations, and options for regulating temperature in the vacuum of space are limited and challenging. To address temperature fluctuations, heaters have traditionally been utilized for maintaining warmth of sensitive electronics. These battery-operated heaters significantly increase the craft’s weight and power usage. Conversely, radiators and reflectors are used to dissipate waste heat and reject thermal loading, respectively, to prevent platform overheating. Depending on mission lifecycle, orbit, and whether the mission is manned or unmanned, the respective ranges of environmental conditions will vary greatly as will the crafts survivability standards. Tailorable and variable thermal management systems are therefore vital to the success of next generation space exploration. To address this issue, Plasmonics Inc. proposes to develop a new class of mission-tailorable, and autoregulating, thermal radiator coatings by leveraging its extensive experience in growing vanadium dioxide (VO2) on flexible substrates. VO2 has been investigated for use in variable emittance regulators in the past; however, in all cases the processing requirements appear to be incompatible with space craft radiator materials. Accordingly, Plasmonics Inc. proposes to design, model, fabricate, and test a range of tungsten-doped vanadium dioxide-base (WxV1-xO2)- variable emissivity materials (VEM). Various concentrations of W will be explored to evaluate its effect on transition temperature and VEM thermal emissivity. After design optimization and testing, the team will fabricate a VEM prototype on flight-certified flexible substrate such as Kapton. Demonstration of a successful flexible VEM this technology can be applied to a wide range of markets with the commercial satellite and smart glass as the most promising.

Technology keywords

Not reported

Other awards by this recipient

Verified by the same UEI. These are other public SBIR/STTR award pages, not a merged company record.

Awards with the same topic code

Verified by an exact topic code match. This is not a text-similarity match.

Research funding history

26 SBIR/STTR records share this UEI (2011–2025). Reported award amounts total $9,171,263. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

Agencies: Department of Defense, National Aeronautics and Space Administration

Agency intelligence

National Aeronautics and Space Administration

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