Howe Industries

Manufacturer United States Verified
5 Products
8 Years Active
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About Howe Industries

Howe Industries was founded by Dr. Troy Howe in the Phoenix metro area to develop advanced propulsion and power technologies for the space sector. Dr. Howe holds a PhD in mechanical engineering from the University of Idaho (2015), with expertise spanning nuclear rocket fuel, thermoelectric converters, solid-state cooling, and space propulsion systems.

The company flagship near-term product is ThermaSat, a solar thermal CubeSat propulsion system developed through NSF SBIR Phase I and II funding. ThermaSat uses water as a non-toxic, green propellant stored as a solid or liquid and vaporized through resistojet heating before being expelled through a nozzle, providing meaningful delta-V for 3U to 12U CubeSat platforms while avoiding the regulatory burden of conventional propellants like hydrazine. The system operates at a minimum of 8 W input power and is scalable with higher power inputs, offering a specific impulse advantage over cold-gas thrusters while maintaining the safe-handling profile critical for university and commercial integrators.

Beyond ThermaSat, Howe Industries has spun out ThermaSat Inc for near-term orbital mobility and ISAM products, while continuing to advance longer-horizon concepts including the Pulsed Plasma Rocket (NASA NIAC Phase II, 2024), the SPRINTR nuclear thermal rocket, the SPEAR deep-space nuclear power probe, and the SEPTIR radioisotope electric thruster. The ROAMER in-space servicing robot was developed through a USSF Orbital Prime STTR award, and the ICARuS coulomb-particle heat radiator enables large-scale nuclear spacecraft designs.

Howe Industries is led by Dr. Troy Howe, who simultaneously serves as CEO of ThermaSat Inc and CTO of Tesseract 4D Energy, bridging near-term CubeSat propulsion products with far-horizon nuclear propulsion research across NASA, NSF, DARPA, and US Space Force programs.

Milestones

  • 2018 Howe Industries founded in Scottsdale, Arizona by Dr. Troy Howe
  • 2019 NSF SBIR Phase I award for ThermaSat CubeSat propulsion system
  • 2020 NASA NIAC Phase I award for Pulsed Plasma Rocket; NASA SBIR Phase I for ATEG Kilopower
  • 2022 NSF SBIR Phase II award for ThermaSat; USSF Orbital Prime STTR for ROAMER servicing robot
  • 2024 NASA NIAC Phase II for Pulsed Plasma Rocket; USSF D2P2 SBIR for ThermaSat+ OTV

Products

5

NASA NIAC-funded nuclear pulsed-plasma propulsion concept aiming to cut crewed Mars transit time to about two months — 100,000 N thrust, 5,000 s specific impulse, 282 MW power.

1 9

Radioisotope-powered electric thruster delivering 3,048 s specific impulse at only 3 W power draw, targeting small satellite and deep space platforms that require long-duration, near-zero power electric propulsion.

1 5

Compact deep-space nuclear power and propulsion probe delivering 3 kW electric at 20% conversion efficiency over a 14-year mission, targeting CubeSat deployment to Europa and other outer solar system destinations.

1 9

Nuclear thermal rocket engine achieving 843 s specific impulse at 9,930 N thrust and 40 MW reactor power, using a scored plate reactor design with liquid hydrogen as propellant.

1 6

Solar thermal CubeSat propulsion system using water as a non-toxic green propellant, delivering resistojet-heated steam thrust for 3U-12U platforms at minimum 8 W input power. NSF SBIR Phase II-funded.

4 6

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