High-Temperature Oscillating Heat Pipes

Pushing the limits of thermal control for aerospace, nuclear, and advanced energy applications requiring heat transfer at high temperatures (~150-500 °C) and ultra-high temperatures temperature (~500-1800 °C)

Testing of an Inconel OHP leading edge

Applications

  • Hypersonic leading edges

  • Nuclear electric propulsion (NEP)

  • Radiator panels

  • Fluid-to-fluid heat exchangers

  • Heat shields

Aerospace

  • Reactor cooling

  • Rejection-side heat rejection

  • Thermoelectric heat transporters

Nuclear

  • Waste heat recovery systems

  • Solar thermal receivers

  • Fuel cells

  • Industrial heat exchangers

  • Semiconductor isothermal liners

  • Breaking system coolers

Industrial & Energy Systems

Publications

Features, Advantages and Benefits of ThermAvant Tech’s OHPs in High Temperature Applications

  • Pressure-driven oscillating two-phase fluid flow, as opposed with capillary-driven like conventional wick-based heat pipes

  • Ultra-high effective thermal conductivities (e.g. 5 to 500x higher than the base material’s)

  • Producible in tubular, flat plate and complex three-dimensional form factors for a variety of applications (e.g., from 10cm to 3m in length and with cross-sectional heights of 1-10mm)

  • 3D structure OHPs have high strength and relatively low density (e.g., 80% effective density of base material with 95% of base material strength)

  • Wide range of fluid-material pairs to operate across wide range of medium- and high-temperatures

ThermAvant Background

2007
Founded by Dr. Bill Ma, Dr. Bin Wu, and Joe Boswell.

2015
First aero-defense prototypes delivered and Dr. Ma published OHP textbook.

2017
First launch of electronics cooling (<100 °C) OHPs on spacecraft on board OTV5, and represents transition of technology to TRL 9.

ThermAvant’s High-Temp Development Timeline

Hypersonics

2019 - 2022

NASA LaRC Phase I-II

2022 - 2025

AFRL/RV Phase III

2023-2025

NASA ARC ACO

2025+

Transitioning into commercial applications

Space Nuclear — Heat Rejection

2020 - 2026

NASA GRC Phase I-III

2024

NASA JPL Phase I

2025+

Transitioning into commercial applications

Space Nuclear — Core Acquisition

2023-2026

NASA GRC Phase I-II

Elevated Temperature OHP Features & Benefits

Proven Thermal Solutions for Mission-Critical Applications

We manage the entire process from concept through manufacturing.

  • World leader in OHP technology with 5 years of experience demonstrating hi-temp solutions (600K to 2,000K)

  • 30+ Engineers dedicated to continuous OHP technology and OHP manufacturing improvements

  • Unique Alkali metal OHP processing capabilities in-house

  • Successfully applied Hi-Temp OHPs (see publications, above)

  • Actively engaged with NASA, DoD, and Primes to apply Hi-Temp OHPs to hypersonic