The Solar Probe Plus solar array development and design

The Solar Probe Plus (SPP) spacecraft will orbit as closely as 9.5 solar radii from the sun; so close that its thermal protection shield (TPS) will reach a peak temperature of 1,400C. To work in this environment, the solar array will use pressurized water cooling and operate in the penumbra formed b...

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Bibliographic Details
Published in2010 35th IEEE Photovoltaic Specialists Conference pp. 000717 - 000722
Main Authors Gaddy, E, Decker, R, Lockwood, M K, Roufberg, L, Knutzen, G, Marsh, D
Format Conference Proceeding
LanguageEnglish
Published IEEE 01.06.2010
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ISBN9781424458905
1424458900
ISSN0160-8371
DOI10.1109/PVSC.2010.5617077

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Summary:The Solar Probe Plus (SPP) spacecraft will orbit as closely as 9.5 solar radii from the sun; so close that its thermal protection shield (TPS) will reach a peak temperature of 1,400C. To work in this environment, the solar array will use pressurized water cooling and operate in the penumbra formed by the TPS at a 68° angle of incidence. Even with these mitigations, the array will be subject to extremely high intensity and temperature. This paper will summarize the array's environment, present a preliminary design, outline development plans and describe phase A test plans. This paper will summarize the array's environment, present a preliminary design, outline development plans and describe phase A test plans.
ISBN:9781424458905
1424458900
ISSN:0160-8371
DOI:10.1109/PVSC.2010.5617077