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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creator | Gaddy, E Decker, R Lockwood, M K Roufberg, L Knutzen, G Marsh, D |
description | 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. |
doi_str_mv | 10.1109/PVSC.2010.5617077 |
format | Conference Proceeding |
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ispartof | 2010 35th IEEE Photovoltaic Specialists Conference, 2010, p.000717-000722 |
issn | 0160-8371 |
language | eng |
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source | IEEE Electronic Library (IEL) Conference Proceedings |
subjects | Arrays Electrostatics Insulators Materials Resistance Sun Trajectory |
title | The Solar Probe Plus solar array development and design |
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