SBIR/STTR Research Award

Venus Energy Converter

Award identifier 85d6ca8dccddc28eedccaa2d5dd29f03f2f92b83d5e3603443138948e35e8b8fAwarding agency National Aeronautics and Space Administration

Award amount

$156,496

Program and phase

SBIR · Phase I

Award year

2025

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
INNOSYS, INC.
Proposal award date
2025-09-23
Contract end date
2026-03-27
UEI
SKSZV1JCCLJ7
Solicitation number
SBIR 2025-I
Topic code
S13

Research abstract

The primary goal is to demonstrate practical, functional power generation sources based on thermionic energy conversion (TEC) capable of operation at extreme temperature environments such as those found on the surface of Venus, propulsion systems and in Long-Lived In-Situ Solar System Explorer (LLISSE) missions. TEC provides an effective way of capturing the abundant source of heat energy found in environments such as Venus and LLISSE. TEC is analogous to solar/photovoltaic (PV) cells with temperature/heat being the energy source for TEC compared to light/optical being the energy source for PV. Unlike thermoelectrics which require and rely on a large temperature difference for operation, TEC can operate with a small or no temperature (isothermal) difference by judiciously using differences in thermionic work functions to convert temperature/heat to electrical energy. Recent advances in material science and nanotechnology as well as the understanding of the underlying physical processes form the basis for this proposed effort to develop Isothermal TECs. This Phase I effort focuses on identifying suitable materials for the creation of the extreme environment TECs and applying the use of integrated circuit, additive manufacturing, and Micro-Electro-Mechanical System (MEMS) technology InnoSys has developed and is developing for, for example, extreme temperature transmitters for Venus to fabricate extreme temperature TECs. Small emitter to collector spacing and properly chosen emissive low work function cathodes and low emission collectors allow conversion of temperature/heat to relatively large electrical current densities at relatively high TEC conversion efficiencies with simple system integration of TECs. Extreme/harsh environment protective packaging will be used. Also, when coupled with sources of heat energy such as radioisotopes and integrated into General Purpose Heat Sources (GPHSs), TEC can be used for planetary and others missions including moon missions.

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

73 SBIR/STTR records share this UEI (2004–2025). Reported award amounts total $33,892,460. Reported amounts are not federal obligations.

Phases: Phase I, Phase II, Phase II – Direct to Phase II

Agencies: Department of Defense, Department of Energy, National Aeronautics and Space Administration

Agency intelligence

National Aeronautics and Space Administration

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