Abstract
We describe a solution for powering a spacecraft in the 5 kW - 0.5 MW power range. The introduced thermo-photovoltaic electricity generation works without magnets or external cooling; it combines operational simplicity with a good power per mass ratio. Once in orbit, the system shall be capable of powering numerous successive missions within the solar system or a long range exploratory mission. © Author(s) 2010.
Cite
CITATION STYLE
APA
Kovacs, A., & Janhunen, P. (2010). Thermo-photovoltaic spacecraft electricity generation. Astrophysics and Space Sciences Transactions, 6(1), 19–26. https://doi.org/10.5194/astra-6-19-2010
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