E3S Web of Conferences (Jan 2017)

Electrical Power Subsystem for the Euclid Spacecraft

  • Ciancetta Ezio,
  • Cimino Marco,
  • Cuzzocrea Giuseppe,
  • Gervasio Giuseppe,
  • Maiorano Elena,
  • Martinez Ignacio,
  • Sanchez Luc

DOI
https://doi.org/10.1051/e3sconf/20171618005
Journal volume & issue
Vol. 16
p. 18005

Abstract

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European Space Agency in the frame of Cosmic Vision 2015-2025 program [ 1 ]. It is a cosmology mission whose prime objective is to study the geometry and the nature of the dark matter and the dark energy with unprecedented accuracy. The spacecraft will be launched in 2020 by a Soyuz launcher, to perform a six-year survey of the extragalactic sky from a large-amplitude orbit around Lagrange point L2 of the Sun-Earth system. This paper outlines the Euclid Electrical Power Subsystem (EPS) design, providing a description of the major design drivers and resulting configuration, with a view to highlight aspects that could be considered for future designs.