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A High Irradiance Peltier Operated Tungsten Exo-Reflector for the daytime exploration of Mercury.

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The Pulsed Plasma Rocket concept. A system that may produce 20,000 lbsf of thrust with an Isp of 5,000 s. The system is derived from the Pulsed Fission Fusion concept but the Pulsed Plasma Rocket (PPR) is smaller, less complex, and more affordable.

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A nuclear thermal rocket for manned exploration of Mars, the Moon, or space colonization.


Nuclear electric propulsion using Advanced Thermoelectric Generators (ATEG)s reaching over 20% efficiency.

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Water based propulsion for CubeSats providing orbit insertion, station keeping for 10 years, and eventual deorbit.

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Low cost, rapid debris de-orbiting for less than $3k per kilogram of removed mass from Earth orbit.

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Howe Industries ThermaSat Video
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Downloads for Additional Information:

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