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Solar Power System Design for the Solar Probe+ Mission
Author(s) -
Geoffrey A. Landis,
J.D. Kinnison,
Martin E. Fraeman,
Lew Roufberg,
Steve Ver,
M. Wirzburger,
Paul Schmitz
Publication year - 2008
Publication title -
6th international energy conversion engineering conference (iecec)
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.2008-5712
Subject(s) - photovoltaic system , solar mirror , solar power , solar radius , solar energy , solar maximum , aerospace engineering , photovoltaic thermal hybrid solar collector , physics , environmental science , coronal mass ejection , power (physics) , solar wind , electrical engineering , engineering , plasma , quantum mechanics
*† ‡ § Solar Probe+ is an ambitious mission proposed to the solar corona, designed to make a perihelion approach of 9 solar radii from the surface of the sun. The high temperature, high solar flux environment makes this mission a significant challenge for power system design. This paper summarizes the power system conceptual design for the solar probe mission. Power supplies considered included nuclear, solar thermoelectric generation, solar dynamic generation using Stirling engines, and solar photovoltaic generation. The solar probe mission ranges from a starting distance from the sun of 1 AU, to a minimum distance of about 9.5 solar radii, or 0.044 AU, from the center of the sun. During the mission, the solar intensity ranges from one to about 510 times AM0. This requires power systems that can operate over nearly three orders of magnitude of incident intensity.

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