Abstract

The thermoradiative cell (TRC) is theoretically investigated, coupled with a radioisotope heat source, to provide primary power for a cubesat mission where photovoltaic power is impractical. Using a representative heat source, such as a single pellet of 238Pu from a General Purpose Heat Source (GPHS), provides 62.5 W of thermal energy. Using the 3K universe as a heat sink and a nominal power conversion efficiency of over 19%, a mass specific power of 30 W/kg is predicted. This represents a order-of-magnitude improvement over conventional radioisotope thermal generators. Realization of practical TRC devices by Metalorganic Vapor Phase Epitaxy (MOVPE), and development of identified low-bandgap materials such as InAs0.91Sb0.09 (0.28 eV) or InP0.63Sb0.37 (0.47 eV), is discussed.

Keywords:
Heat sink Gallium arsenide Energy conversion efficiency Materials science Photovoltaic system Nuclear engineering Optoelectronics Electricity generation Generator (circuit theory) Solar cell Thermal Power (physics) Electrical engineering Physics Engineering Thermodynamics

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Citation History

Topics

Advanced Thermoelectric Materials and Devices
Physical Sciences →  Materials Science →  Materials Chemistry
Advanced Energy Technologies and Civil Engineering Innovations
Physical Sciences →  Energy →  Nuclear Energy and Engineering
solar cell performance optimization
Physical Sciences →  Engineering →  Electrical and Electronic Engineering
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