TY - GEN
T1 - The FIREBall-2 UV balloon telescope
T2 - UV, X-Ray, and Gamma-Ray Space Instrumentation for Astronomy XXI 2019
AU - Hoadley, Keri
AU - Hamden, Erika T.
AU - Milliard, Bruno
AU - Khan, Aafaque R.
AU - Agarwal, Simran
AU - Lin, Zeren
AU - Schiminovich, David
AU - Kyne, Gillian
AU - Evrard, Jean
AU - Martin, D. Christopher
N1 - Publisher Copyright:
© COPYRIGHT SPIE. Downloading of the abstract is permitted for personal use only.
PY - 2019
Y1 - 2019
N2 - 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 ∼ 0.3 (C IV); z ∼ 0.7 (Lyα); z ∼ 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-flight. 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.
AB - 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 ∼ 0.3 (C IV); z ∼ 0.7 (Lyα); z ∼ 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-flight. 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.
KW - CGM
KW - Galaxy Evolution
KW - Optical Alignment
KW - Scientific Ballooning
UR - http://www.scopus.com/inward/record.url?scp=85076910846&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=85076910846&partnerID=8YFLogxK
U2 - 10.1117/12.2530047
DO - 10.1117/12.2530047
M3 - Conference contribution
AN - SCOPUS:85076910846
T3 - Proceedings of SPIE - The International Society for Optical Engineering
BT - UV, X-Ray, and Gamma-Ray Space Instrumentation for Astronomy XXI
A2 - Siegmund, Oswald H.
PB - SPIE
Y2 - 11 August 2019 through 13 August 2019
ER -