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EOS-AM Solar Array Arc Mitigation Design
ISSN: 0148-7191, e-ISSN: 2688-3627
Published August 02, 1999 by SAE International in United States
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This paper discusses the design and test program initiated to retrofit the EOS-AM solar array, protecting it from a newly discovered damage mechanism that is initiated by electrostatic discharges (ESD) while in orbit.
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CitationDavis, S., Stillwell, R., Andiario, W., Snyder, D. et al., "EOS-AM Solar Array Arc Mitigation Design," SAE Technical Paper 1999-01-2582, 1999, https://doi.org/10.4271/1999-01-2582.
- Katz, I. Davis, V.A. and Snyder, D.B. “Mechanism for Spacecraft Charging Initiated Destruction of Solar Arrays in GEO,” AIAA Paper 98-1002, January 1998.
- Hoeber, C.F. Robertson, E.A. Katz, I. Davis, V.A. and Snyder, D.B. “Solar Array Augmented Electrostatic Discharge in GEO, ” AIAA Paper 98-1401, February1998.
- Herriage, M.J. Kurland, R.M. Faust, C.D. Gaddy, E.M. and Keys, D.J. “EOS AM-a GaAS/Ge Flexible Blanket Solar Array Verification Test Program Results” Proceeding, 32nd Intersociety Energy Conversion Engineering Conference, Honolulu, HI, Vol. 1 pp 556-562, 1997.
- Herriage, M.J. Kurland, R.M. Faust, C.D. Gaddy, E.M. and Keys, D.J. “EOS AM-a GaAS/Ge Flexible Blanket Solar Array ”Proceeding, 31st Intersociety Energy Conversion Engineering Conference, Washington DC, Vol. 1 pp 56-62, 1997.