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    The FIREBall-2 UV balloon telescope: 2018 flight and improvements for 2020

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    Author
    Hoadley, Keri
    Hamden, Erika T.
    Milliard, Bruno
    Khan, Aafaque
    Agarwal, Simran
    Lin, Zeren
    Schiminovich, David
    Kyne, Gillian
    Evrard, Jean
    Martin, Christopher
    Affiliation
    Univ Arizona, Steward Observ
    Issue Date
    2019-09-09
    Keywords
    Scientific Ballooning
    CGM
    Galaxy Evolution
    Optical Alignment
    
    Metadata
    Show full item record
    Publisher
    SPIE-INT SOC OPTICAL ENGINEERING
    Citation
    Keri Hoadley, Erika T. Hamden, Bruno Milliard, Aafaque R. Khan, Simran Agarwal, Zeren Lin, David Schiminovich, Gillian Kyne, Jean Evrard, and D. Christopher Martin "The FIREBall-2 UV balloon telescope: 2018 flight and improvements for 2020", Proc. SPIE 11118, UV, X-Ray, and Gamma-Ray Space Instrumentation for Astronomy XXI, 1111815 (9 September 2019); https://doi.org/10.1117/12.2530047
    Journal
    UV, X-RAY, AND GAMMA-RAY SPACE INSTRUMENTATION FOR ASTRONOMY XXI
    Rights
    Copyright © 2019 SPIE.
    Collection Information
    This item from the UA Faculty Publications collection is made available by the University of Arizona with support from the University of Arizona Libraries. If you have questions, please contact us at repository@u.library.arizona.edu.
    Abstract
    The Faint Intergalactic-medium Redshifted Emission Balloon (FIREBall-2, FB-2) is designed to discover and map faint UV emission from the circumgalactic medium around low redshift galaxies (z similar to 0.3 (C IV); z similar to 0.7 (Lyff); z similar to 1.0 (O VI)). FIREBall-2's first launch, on September 22nd 2018 out of Ft. Sumner, NM, was abruptly cut short due to a hole that developed in the balloon. FIREBall-2 was unable to observe above its minimum require altitude (25 km; nominal: 32 km) for its shortest required time (2 hours; nominal: 8+ hours). The shape of the deflated balloon, as well as a concurrent full moon close to our observed target field, revealed a severe, off-axis scattered light path directly to the UV science detector. Additional damage to FB-2 added complications to the ongoing effort to prepare FB-2 for a quick re-floght. Upon landing, several mirrors in the optical chain, including the two large telescope mirrors, were damaged, resulting in chunks of material broken off the sides and reflecting surfaces. The magnifying optical element, called the focal corrector, was discovered to be misaligned beyond tolerance after the 2018 flight, with one of its two mirrors damaged from the landing impact. We describe the steps taken thus far to mitigate the damage to the optics, as well as procedures and results from the ongoing efforts to re-align the focal corrector and spectrograph optics. We report the throughput of the spectrograph before and after the 2018 flight and plans for improving it. Finally, we describe several methods by which we address the scattered light issues seen from FIREBall-2's 2018 campaign and present the current status of FB-2 to fly during the summer campaign in Palestine, TX in 2020.
    ISSN
    0277-786X
    DOI
    10.1117/12.2530047
    Version
    Final published version
    ae974a485f413a2113503eed53cd6c53
    10.1117/12.2530047
    Scopus Count
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    UA Faculty Publications

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