DocumentCode
2784519
Title
The Solar Probe Plus solar array development and design
Author
Gaddy, Edward ; Decker, Rob ; Lockwood, Mary Kae ; Roufberg, Lew ; Knutzen, Gayle ; Marsh, Danielle
Author_Institution
Appl. Phys. Lab., Johns Hopkins Univ., Laurel, MD, USA
fYear
2010
fDate
20-25 June 2010
Abstract
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.
Keywords
solar cell arrays; solar heating; space vehicles; thermal resistance; pressurized water cooling; solar array; solar probe plus spacecraft; temperature 1400 C; thermal protection shield; Arrays; Electrostatics; Insulators; Materials; Resistance; Sun; Trajectory;
fLanguage
English
Publisher
ieee
Conference_Titel
Photovoltaic Specialists Conference (PVSC), 2010 35th IEEE
Conference_Location
Honolulu, HI
ISSN
0160-8371
Print_ISBN
978-1-4244-5890-5
Type
conf
DOI
10.1109/PVSC.2010.5617077
Filename
5617077
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