Translator Disclaimer
4 March 2020 Design and construction of the x-ray instrumentation onboard the HaloSat CubeSat
Author Affiliations +
Abstract

HaloSat is the first mission funded by NASA’s Astrophysics Division to use the CubeSat platform. Using three co-aligned silicon drift detectors, the HaloSat observatory measures soft (0.4 to 7 keV) x-ray emission from sources of diffuse emission such as the hot, gaseous halo of the Milky Way. We describe the design and construction of the science payload on HaloSat and the reasoning behind many of the choices. As a direct result of the design choices and adherence to best practices during construction, the HaloSat science payload continues to perform well after more than one year on-orbit.

© 2020 Society of Photo-Optical Instrumentation Engineers (SPIE) 2329-4124/2020/$28.00 © 2020 SPIE
Daniel M. LaRocca, Philip Kaaret, Donald L. Kirchner, Anna Zajczyk, William Robison, Thomas E. Johnson, Keith M. Jahoda, William Fuelberth, Hannah C. Gulick, Ross McCurdy, Keith White, and Drew M. Miles "Design and construction of the x-ray instrumentation onboard the HaloSat CubeSat," Journal of Astronomical Telescopes, Instruments, and Systems 6(1), 014003 (4 March 2020). https://doi.org/10.1117/1.JATIS.6.1.014003
Received: 18 November 2019; Accepted: 19 February 2020; Published: 4 March 2020
JOURNAL ARTICLE
14 PAGES


SHARE
Advertisement
Advertisement
RELATED CONTENT

Caliste SO the x ray spectrometer unit of the...
Proceedings of SPIE (July 23 2014)
Silicon drift chamber with extended energy range
Proceedings of SPIE (December 13 2000)
The use of small x ray detectors for deep space...
Proceedings of SPIE (October 15 2012)

Back to Top