Abstract

Relativistic electrons (E > 1 MeV) cause internal charging on satellites and are an important space weather hazard. A key requirement in space weather research concerns extreme events and knowledge of the largest flux expected to be encountered over the lifetime of a satellite mission. This is interesting both from scientific and practical points of view since satellite operators, engineers, and the insurance industry need this information to better evaluate the effects of extreme events on their spacecraft. Here we conduct an extreme value analysis of daily averaged E > 2 MeV electron fluxes from the Geostationary Operational Environmental Satellites (GOES) during the 19.5 year period from 1 January 1995 to 30 June 2014. We find that the daily averaged flux measured at GOES West is typically a factor of about 2.5 higher than that measured at GOES East, and we conduct independent analyses for these two locations. The 1 in 10, 1 in 50, and 1 in 100 year daily averaged E > 2 MeV electron fluxes at GOES West are 1.84 ×105, 5.00 ×105, and 7.68 ×105 cm−2 s−1 sr−1, respectively. The corresponding fluxes at GOES East are 6.53 ×104, 1.98 ×105, and 3.25 ×105 cm−2 s−1 sr−1, respectively. The largest fluxes seen during the 19.5 year period on 29 July 2004 were particularly extreme and were seen by satellites at GOES West and GOES East. The extreme value analysis suggests that this event was a 1 in 50 year event.

Highlights

  • Space weather is an increasingly important natural hazard risk as society becomes ever more heavily dependent on satellite technology for communications, navigation, defense, and Earth observation [e.g., Horne et al, 2013]

  • We find that the daily averaged flux measured at Geostationary Operational Environmental Satellites (GOES) West is typically a factor of about 2.5 higher than that measured at GOES East, and we conduct independent analyses for these two locations

  • The daily averaged flux measured at GOES West is typically a factor of ∼2.5 higher than that measured at GOES East

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Summary

Introduction

Space weather is an increasingly important natural hazard risk as society becomes ever more heavily dependent on satellite technology for communications, navigation, defense, and Earth observation [e.g., Horne et al, 2013]. The impacts of space weather on satellite operations range from momentary interruptions of service to a total loss of capabilities when a satellite fails. Other satellite losses and partial losses that have been associated with adverse space weather conditions include Anik E2 on 20 January 1994 [Baker, 2001], Telstar 401 on 11 January 1997 [Lanzerotti et al, 1998], Galaxy 10R on 3 August 2004 [Choi et al, 2011], Intelsat 804 on January 2005 [Royal Academy of Engineering Report, 2013], and Galaxy on 5 April 2010 [Allen, 2010]. There is a large uncertainty associated with this estimate, and the likely effect of a severe space weather storm on the satellite fleet remains difficult to quantify

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