SBIR/STTR Research Award

Oscillating Heat Pipe Enhanced Thermal Wadi

Award identifier 22bcbcd8f941b3bf87d43bde5a90caf6b305ba059a0d6a73d3c2633196629f9bAwarding agency National Aeronautics and Space Administration

Award amount

$120,873

Program and phase

SBIR · Phase I

Award year

2020

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
THERMAVANT TECHNOLOGIES LLC
Proposal award date
2020-08-25
Contract end date
2021-03-01
UEI
HNM9C3HMA9H4
Solicitation number
SBIR_20_P1
Topic code
S3

Research abstract

NASA is seeking innovative approaches and techniques fornbsp;lunar surface payload survival.nbsp; This payload must survive the large temperature swings of the lunar diurnal cycle and the challenging lunar thermal environment. This lunar environment poses significant difficulties to small, low power (le;100W) payloads, rovers, and landers required for lunar science, especially in the absence of perpetual power supplies, while still demanding operability for many lunar cycles in the extreme lunar environment. To achieve these goals, ThermAvant Technologies, LLC proposes developing a system of interconnected Oscillating Heat Pipes (OHPs) to enable an enhanced thermal wadi. Essentially, the lunar wadi concept is to create a thermal mass by solidifying loose lunar regolith and configuring this mass such that it can be heated during the lunar day and can provide sufficient heat during the lunar night to maintain lunar rovers and other payload equipment above their minimum survival temperatures. An OHP-enhanced thermal wadi is envisioned that takes advantage of completely burying the thermal mass in lunar regolith and using OHPs to capture and transport the heat for storage (Hot Sink), for rover warming (Parking Plate), and, independently, for power generation (Heat Engine).The OHP-based Hot Sink will provide unique features not found in a state-of-the-art thermal wadi by demonstrating OHPs functioning as variable conductance devices integrated as thermal switches, variable heat flux acquisition and heat load capability depending on temperature demands, application-specific working fluids capable of operating over the extreme lunar temperature conditions, improved effective thermal conductivity, structural body form factor for improved thermal resistance with reduced mass, and gravity independent performance.

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.

Research funding history

44 SBIR/STTR records share this UEI (2009–2025). Reported award amounts total $21,824,921. Reported amounts are not federal obligations.

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

Agencies: Department of Defense, National Aeronautics and Space Administration, National Science Foundation

Agency intelligence

National Aeronautics and Space Administration

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