DocumentCode :
2563019
Title :
LEO spacecraft leakage current and discharging phenomena: TRW LDEF SP-HVDE (space plasma-high voltage drainage experiment)
Author :
Yaung, J.Y. ; Wong, W.C. ; Blakkolb, B.K. ; Ryan, L.E. ; Taylor, W.W.L.
Author_Institution :
TRW, Redondo Beach, CA, USA
fYear :
1991
fDate :
7-11 Oct 1991
Firstpage :
1566
Abstract :
Two identical SP-HVDE solar cell trays were flown in the NASA 5.75-year LDEF (Long Duration Exposure Facility), one near the leading edge and the other near the trailing edge, in the LEO (low Earth orbit) environment. Each experiment tray consisted of six assemblies with each made of Kapton dielectric samples of varying thickness (i.e., 2 mils, 3 mils, and 5 mils) biased under ±300 V, ±500 V, and ±1000 V. The objectives have been successfully achieved by measuring the first post-flight long-term (i.e. roughly 8-month experiment) average leakage current through 95% measurable coulombmeters and surface materials
Keywords :
leakage currents; solar cell arrays; space vehicle power plants; 1000 V; 2 mm; 3 mm; 300 V; 5 mm; 500 V; Kapton dielectric samples; Long Duration Exposure Facility; NASA; coulombmeters; discharging phenomena; leakage current; solar cells; space plasma-high voltage drainage experiment; spacecraft; surface materials; Current measurement; Dielectric measurements; Extraterrestrial measurements; Lead; Leakage current; Low earth orbit satellites; NASA; Photovoltaic cells; Space vehicles; Thickness measurement;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Photovoltaic Specialists Conference, 1991., Conference Record of the Twenty Second IEEE
Conference_Location :
Las Vegas, NV
Print_ISBN :
0-87942-636-5
Type :
conf
DOI :
10.1109/PVSC.1991.169467
Filename :
169467
Link To Document :
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