Space Science Reviews

, Volume 141, Issue 1, pp 171–184

The THEMIS Magnetic Cleanliness Program

Authors

    • Space Sciences LaboratoryUniversity of California
  • V. Angelopoulos
    • Space Sciences LaboratoryUniversity of California
    • IGPP/ESSUniversity of California
  • E. Taylor
    • Space Sciences LaboratoryUniversity of California
  • R. C. Snare
    • IGPP/ESSUniversity of California
  • J. D. Means
    • IGPP/ESSUniversity of California
  • Y. S. Ge
    • IGPP/ESSUniversity of California
  • P. Narvaez
    • NASA/JPL
  • H. U. Auster
    • TUBS
  • O. Le Contel
    • CETP/IPSL
  • D. Larson
    • Space Sciences LaboratoryUniversity of California
  • T. Moreau
    • Space Sciences LaboratoryUniversity of California
Article

DOI: 10.1007/s11214-008-9423-3

Cite this article as:
Ludlam, M., Angelopoulos, V., Taylor, E. et al. Space Sci Rev (2008) 141: 171. doi:10.1007/s11214-008-9423-3

Abstract

The five identical THEMIS Spacecraft, launched in February 2007, carry two magnetometers on each probe, one DC fluxgate (FGM) and one AC search coil (SCM). Due to the small size of the THEMIS probes, and the short length of the magnetometer booms, magnetic cleanliness was a particularly complex task for this medium sized mission. The requirements leveled on the spacecraft and instrument design required a detailed approach, but one that did not hamper the development of the probes during their short design, production and testing phase. In this paper we describe the magnetic cleanliness program’s requirements, design guidelines, program implementation, mission integration and test philosophy and present test results, and mission on-orbit performance.

Keywords

THEMISMagnetic cleanlinessSpacecraft cleanliness

PACS

94.05.-a94.80.+g95.40.+s07.87.+v

Copyright information

© Springer Science+Business Media B.V. 2008