Progress on the Micro-X rocket payload

The Micro-X High Resolution Microcalorimeter X-ray Imaging Rocket is sounding rocket experiment that will combine a transition-edge-sensor X-ray-microcalorimeter array with a conical imaging mirror to obtain high-spectral-resolution images of extended and point X-ray sources. Our first target is the...

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Main Authors: Schulz, Norbert S., Leman, Steven W., Kissel, Steve E., Flanagan, Kathryn A., Wikus, Patrick, Bautz, Marshall W., Figueroa-Feliciano, Enectali, Rutherford, J., Levine, Alan M
Other Authors: Massachusetts Institute of Technology. Department of Physics
Format: Article
Language:en_US
Published: The International Society for Optical Engineering 2010
Online Access:http://hdl.handle.net/1721.1/52665
https://orcid.org/0000-0002-1379-4482
https://orcid.org/0000-0001-9285-5556
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author Schulz, Norbert S.
Leman, Steven W.
Kissel, Steve E.
Flanagan, Kathryn A.
Wikus, Patrick
Bautz, Marshall W.
Figueroa-Feliciano, Enectali
Rutherford, J.
Levine, Alan M
author2 Massachusetts Institute of Technology. Department of Physics
author_facet Massachusetts Institute of Technology. Department of Physics
Schulz, Norbert S.
Leman, Steven W.
Kissel, Steve E.
Flanagan, Kathryn A.
Wikus, Patrick
Bautz, Marshall W.
Figueroa-Feliciano, Enectali
Rutherford, J.
Levine, Alan M
author_sort Schulz, Norbert S.
collection MIT
description The Micro-X High Resolution Microcalorimeter X-ray Imaging Rocket is sounding rocket experiment that will combine a transition-edge-sensor X-ray-microcalorimeter array with a conical imaging mirror to obtain high-spectral-resolution images of extended and point X-ray sources. Our first target is the Puppis A supernova remnant, which will be observed in January 2011. The Micro-X observation of the bright eastern knot of Puppis A will obtain a line-dominated spectrum with up to 90,000 counts collected in 300 seconds at 2 eV resolution across the 0.3-2.5 keV band. Micro-X will utilize plasma diagnostics to determine the thermodynamic and ionization state of the plasma, to search for line shifts and broadening associated with dynamical processes, and seek evidence of ejecta enhancement. We describe the progress made in developing this payload, including the detector, cryogenics, and electronics assemblies. A detailed modeling effort has been undertaken to design a rocket-bourne adiabatic demagnetization refrigerator with sufficient magnetic shielding to allow stable operation of transition edge sensors, and the associated rocket electronics have been prototyped and tested.
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spelling mit-1721.1/526652022-09-27T20:14:37Z Progress on the Micro-X rocket payload Schulz, Norbert S. Leman, Steven W. Kissel, Steve E. Flanagan, Kathryn A. Wikus, Patrick Bautz, Marshall W. Figueroa-Feliciano, Enectali Rutherford, J. Levine, Alan M Massachusetts Institute of Technology. Department of Physics Massachusetts Institute of Technology. School of Science MIT Kavli Institute for Astrophysics and Space Research Figueroa-Feliciano, Enectali Schulz, Norbert S. Rutherford, John Morton Levine, Alan M. Leman, Steven W. Kissel, Steve E. Flanagan, Kathryn A. Wikus, Patrick Bautz, Marshall W. Figueroa-Feliciano, Enectali The Micro-X High Resolution Microcalorimeter X-ray Imaging Rocket is sounding rocket experiment that will combine a transition-edge-sensor X-ray-microcalorimeter array with a conical imaging mirror to obtain high-spectral-resolution images of extended and point X-ray sources. Our first target is the Puppis A supernova remnant, which will be observed in January 2011. The Micro-X observation of the bright eastern knot of Puppis A will obtain a line-dominated spectrum with up to 90,000 counts collected in 300 seconds at 2 eV resolution across the 0.3-2.5 keV band. Micro-X will utilize plasma diagnostics to determine the thermodynamic and ionization state of the plasma, to search for line shifts and broadening associated with dynamical processes, and seek evidence of ejecta enhancement. We describe the progress made in developing this payload, including the detector, cryogenics, and electronics assemblies. A detailed modeling effort has been undertaken to design a rocket-bourne adiabatic demagnetization refrigerator with sufficient magnetic shielding to allow stable operation of transition edge sensors, and the associated rocket electronics have been prototyped and tested. 2010-03-17T16:40:50Z 2010-03-17T16:40:50Z 2008-07 Article http://purl.org/eprint/type/JournalArticle 0277-786X http://hdl.handle.net/1721.1/52665 Figueroa-Feliciano, E. et al. “Progress on the Micro-X rocket payload.” Space Telescopes and Instrumentation 2008: Ultraviolet to Gamma Ray. Ed. Martin J. L. Turner & Kathryn A. Flanagan. Marseille, France: SPIE, 2008. 70113U-10. © 2008 SPIE--The International Society for Optical Engineering https://orcid.org/0000-0002-1379-4482 https://orcid.org/0000-0001-9285-5556 en_US http://dx.doi.org/10.1117/12.789904 Proceedings of SPIE Article is made available in accordance with the publisher's policy and may be subject to US copyright law. Please refer to the publisher's site for terms of use. application/pdf The International Society for Optical Engineering SPIE
spellingShingle Schulz, Norbert S.
Leman, Steven W.
Kissel, Steve E.
Flanagan, Kathryn A.
Wikus, Patrick
Bautz, Marshall W.
Figueroa-Feliciano, Enectali
Rutherford, J.
Levine, Alan M
Progress on the Micro-X rocket payload
title Progress on the Micro-X rocket payload
title_full Progress on the Micro-X rocket payload
title_fullStr Progress on the Micro-X rocket payload
title_full_unstemmed Progress on the Micro-X rocket payload
title_short Progress on the Micro-X rocket payload
title_sort progress on the micro x rocket payload
url http://hdl.handle.net/1721.1/52665
https://orcid.org/0000-0002-1379-4482
https://orcid.org/0000-0001-9285-5556
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