The FIREBall-2 UV balloon telescope: 2018 flight and improvements for 2020
Author
Hoadley, KeriHamden, Erika T.
Milliard, Bruno
Khan, Aafaque
Agarwal, Simran
Lin, Zeren
Schiminovich, David
Kyne, Gillian
Evrard, Jean
Martin, Christopher
Affiliation
Univ Arizona, Steward ObservIssue Date
2019-09-09
Metadata
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SPIE-INT SOC OPTICAL ENGINEERINGCitation
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/10.1117/12.2530047Rights
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
0277-786XVersion
Final published versionae974a485f413a2113503eed53cd6c53
10.1117/12.2530047