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The solar and heliospheric imager (SoloHI) instrument for the solar orbiter mission

Authors :
Simon Plunkett
M. T. Carter
Dennis G. Socker
James Robert Janesick
Pierre Rochus
D. H. Chua
Clarence M. Korendyke
E. M. DeJong
N. Rich
John Robertson Tower
Adam Thurn
David Keller
Volker Bothmer
D. R. McMullin
Marco Velli
Russell A. Howard
Greg Clifford
Mark G. Linton
Jean-Philippe Halain
William Bast
Arnaud Thernisien
P. C. Liewer
Angelos Vourlidas
Mark Grygon
Philippe Lamy
R. Hagood
Dennis Wang
Zoran Mikic
Sean Lynch
Source :
Solar Physics and Space Weather Instrumentation V.
Publication Year :
2013
Publisher :
SPIE, 2013.

Abstract

The SoloHI instrument for the ESA/NASA Solar Orbiter mission will track density fluctuations in the inner heliosphere, by observing visible sunlight scattered by electrons in the solar wind. Fluctuations are associated with dynamic events such as coronal mass ejections, but also with the “quiescent” solar wind. SoloHI will provide the crucial link between the low corona observations from the Solar Orbiter instruments and the in-situ measurements on Solar Orbiter and the Solar Probe Plus missions. The instrument is a visible-light telescope, based on the SECCHI/Heliospheric Imager (HI) currently flying on the STEREO mission. In this concept, a series of baffles reduce the scattered light from the solar disk and reflections from the spacecraft to levels below the scene brightness, typically by a factor of 10 12 . The fluctuations are imposed against a much brighter signal produced by light scattered by dust particles (the zodiacal light/F-corona). Multiple images are obtained over a period of several minutes and are summed on-board to increase the signal-to-noise ratio and to reduce the telemetry load. SoloHI is a single telescope with a 40⁰ field of view beginning at 5⁰ from the Sun center. Through a series of Venus gravity assists, the minimum perihelia for Solar Orbiter will be reduced to about 60 Rsun (0.28 AU), and the inclination of the orbital plane will be increased to a maximum of 35⁰ after the 7 year mission. The CMOS/APS detector is a mosaic of four 2048 x 1920 pixel arrays, each 2-side buttable with 11 µm pixels.

Details

ISSN :
0277786X
Database :
OpenAIRE
Journal :
Solar Physics and Space Weather Instrumentation V
Accession number :
edsair.doi...........3e35d3b58a7b36c85e93258305d75919
Full Text :
https://doi.org/10.1117/12.2027657