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Solar Power System Design for the Solar Probe+ MissionSolar 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.
Document ID
20090004577
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Landis, Geoffrey A.
(NASA Glenn Research Center Cleveland, OH, United States)
Schmitz, Paul C.
(NASA Glenn Research Center Cleveland, OH, United States)
Kinnison, James
(Johns Hopkins Univ. Laurel, MD, United States)
Fraeman, Martin
(Johns Hopkins Univ. Laurel, MD, United States)
Roufberg, Lew
(Johns Hopkins Univ. Laurel, MD, United States)
Vernon, Steve
(Johns Hopkins Univ. Laurel, MD, United States)
Wirzburger, Melissa
(Johns Hopkins Univ. Laurel, MD, United States)
Date Acquired
August 24, 2013
Publication Date
July 28, 2008
Subject Category
Solar Physics
Report/Patent Number
E-16841
AIAA Paper-2008-5712
Meeting Information
Meeting: 6th International Energy Conversion Engineering Conference (IECEC)
Location: Cleveland, OH
Country: United States
Start Date: July 28, 2008
End Date: July 30, 2008
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 937818.01.01.10
Distribution Limits
Public
Copyright
Public Use Permitted.
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