CUBESPEC: low-cost space-based astronomical spectroscopy

Authors
  • G. Raskin
  • T. Delabie
  • W. De Munter
  • H. Sana
  • B. Vandenbussche
  • B. Vandoren
  • V. Antoci
  • H. Kjeldsen
  • C. Karoff
  • A. de Koter
  • J.-M. Désert ORCID logo
  • T. Mladenov
  • D. Vandepitte
Publication date 2018
Host editors
  • M. Lystrup
  • H.A. MacEwen
  • G.G. Fazio
Book title Space Telescopes and Instrumentation 2018: Optical, Infrared, and Millimeter Wave
Book subtitle 10-15 June 2018, Austin, Texas, United States
ISBN
  • 9781510619494
ISBN (electronic)
  • 9781510619500
Series Proceedings of the SPIE
Event Space Telescopes and Instrumentation 2018
Article number 106985R
Volume | Issue number 3
Number of pages 12
Publisher Bellingham, WA: SPIE
Organisations
  • Faculty of Science (FNWI) - Anton Pannekoek Institute for Astronomy (API)
Abstract
CubeSats are routinely used for low-cost photometry from space. Space-borne spectroscopy, however, is still the exclusive domain of much larger platforms. Key astrophysical questions in e.g. stellar physics and exoplanet research require uninterrupted spectral monitoring from space over weeks or months. Such monitoring of individual sources is unfortunately not affordable with these large platforms. With CUBESPEC we plan to offer the astronomical community a low-cost CubeSat solution for near-UV/optical/near-IR spectroscopy that enables this type of observations.
CUBESPEC is a generic spectrograph that can be configured with minimal hardware changes to deliver both low resolution (R = 100) with very large spectral coverage (200 - 1000 nm), as well as high resolution (R = 30 000) over a selected wavelength range. It is built around an off-axis Cassegrain telescope and a slit spectrograph with configurable dispersion elements. CUBESPEC will use a compact attitude determination and control system for coarse pointing of the entire spacecraft, supplemented with a fine-guidance system using a fast steering mirror to center the source on the spectrograph slit and to cancel out satellite jitter. An extremely compact optical design allows us to house this instrument in a 6U CubeSat with a volume of only 10 × 20 × 30 cm3 , while preserving a maximized entrance pupil of ca. 9 × 19 cm2 . In this contribution, we give an overview of the CUBESPEC project, discuss its most relevant science cases, and present the design of the instrument.
Document type Conference contribution
Language English
Published at https://doi.org/10.1117/12.2314074
Other links http://adsabs.harvard.edu/abs/2018SPIE10698E..5RR
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