TY - GEN
T1 - A next generation Ultra-Fast Flash Observatory (UFFO-100) for IR/optical observations of the rise phase of gamma-ray bursts
AU - Grossan, B.
AU - Park, I.H.
AU - Ahmad, S.
AU - Ahn, K.B.
AU - Barrillon, P.
AU - Brandt, Søren
AU - Budtz-Jørgensen, Carl
AU - Castro-Tirado, A.J.
AU - Chen, P.
AU - Choi, H.S.
AU - Choi, J.
AU - Connell, P.
AU - Dagoret-Campagne, S.
AU - De La Taille, C.
AU - Eyles, C.
AU - Hermann, I.
AU - Huang, M.-H. A.
AU - Jung, A.
AU - Jeong, S.
AU - Kim, J. E.
AU - Kim, M.
AU - Kim, S.-W.
AU - Kim, Y. W.
AU - Lee, J.
AU - Lim, H.
AU - Linder, E. V.
AU - Liu, T._C.
AU - Lund, Niels
AU - Min, K. W.
AU - Na, G. W.
AU - Nam, J. W.
AU - Panasyuk, M. I.
AU - Ripa, J.
AU - Reglero, V.
AU - Rodrigo, J. M.
AU - Smoot, G. F.
AU - Suh, J. E.
AU - Svertilov, S.
AU - Vedenkin, N.
AU - Wang, M._Z.
AU - Yashin, I.
AU - Zhao, M. H.
N1 - Conference code: 8443
PY - 2012
Y1 - 2012
N2 - The Swift Gamma-ray Burst (GRB) observatory responds to GRB triggers with optical observations in ~ 100 s, butcannot respond faster than ~ 60 s. While some rapid-response ground-based telescopes have responded quickly, thenumber of sub-60 s detections remains small. In 2013 June, the Ultra-Fast Flash Observatory-Pathfinder is expected tobe launched on the Lomonosov spacecraft to investigate early optical GRB emission. Though possessing uniquecapability for optical rapid-response, this pathfinder mission is necessarily limited in sensitivity and event rate; here wediscuss the next generation of rapid-response space observatory instruments. We list science topics motivating ourinstruments, those that require rapid optical-IR GRB response, including: A survey of GRB rise shapes/times,measurements of optical bulk Lorentz factors, investigation of magnetic dominated (vs. non-magnetic) jet models,internal vs. external shock origin of prompt optical emission, the use of GRBs for cosmology, and dust evaporation inthe GRB environment. We also address the impacts of the characteristics of GRB observing on our instrument andobservatory design. We describe our instrument designs and choices for a next generation space observatory as a secondinstrument on a low-earth orbit spacecraft, with a 120 kg instrument mass budget. Restricted to relatively modest mass,power, and launch resources, we find that a coded mask X-ray camera with 1024 cm2 of detector area could rapidlylocate about 64 GRB triggers/year. Responding to the locations from the X-ray camera, a 30 cm aperture telescope witha beam-steering system for rapid (~ 1 s) response and a near-IR camera should detect ~ 29 GRB, given Swift GRBproperties. The additional optical camera would permit the measurement of a broadband optical-IR slope, allowingbetter characterization of the emission, and dynamic measurement of dust extinction at the source, for the first time.© (2012) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
AB - The Swift Gamma-ray Burst (GRB) observatory responds to GRB triggers with optical observations in ~ 100 s, butcannot respond faster than ~ 60 s. While some rapid-response ground-based telescopes have responded quickly, thenumber of sub-60 s detections remains small. In 2013 June, the Ultra-Fast Flash Observatory-Pathfinder is expected tobe launched on the Lomonosov spacecraft to investigate early optical GRB emission. Though possessing uniquecapability for optical rapid-response, this pathfinder mission is necessarily limited in sensitivity and event rate; here wediscuss the next generation of rapid-response space observatory instruments. We list science topics motivating ourinstruments, those that require rapid optical-IR GRB response, including: A survey of GRB rise shapes/times,measurements of optical bulk Lorentz factors, investigation of magnetic dominated (vs. non-magnetic) jet models,internal vs. external shock origin of prompt optical emission, the use of GRBs for cosmology, and dust evaporation inthe GRB environment. We also address the impacts of the characteristics of GRB observing on our instrument andobservatory design. We describe our instrument designs and choices for a next generation space observatory as a secondinstrument on a low-earth orbit spacecraft, with a 120 kg instrument mass budget. Restricted to relatively modest mass,power, and launch resources, we find that a coded mask X-ray camera with 1024 cm2 of detector area could rapidlylocate about 64 GRB triggers/year. Responding to the locations from the X-ray camera, a 30 cm aperture telescope witha beam-steering system for rapid (~ 1 s) response and a near-IR camera should detect ~ 29 GRB, given Swift GRBproperties. The additional optical camera would permit the measurement of a broadband optical-IR slope, allowingbetter characterization of the emission, and dynamic measurement of dust extinction at the source, for the first time.© (2012) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
KW - Gamma-ray bursts
KW - X-ray instrumentation
KW - Space astrophysics missions
KW - Space astrophysics instrumentation
KW - Ultra-fast flash observatory (UFFO)
U2 - 10.1117/12.926391
DO - 10.1117/12.926391
M3 - Conference article
SN - 0277-786X
VL - 8443
SP - 84432R
JO - Proceedings of SPIE - The International Society for Optical Engineering
JF - Proceedings of SPIE - The International Society for Optical Engineering
T2 - SPIE Astronomical Telescopes + Instrumentation 2012
Y2 - 1 July 2012 through 6 July 2012
ER -