TY - JOUR
T1 - Flight model characterization of the wide-field off-axis telescope for the MATS satellite
AU - Park, Woojin
AU - Hammar, Arvid
AU - Pak, Soojong
AU - Chang, Seunghyuk
AU - Gumbel, Jörg
AU - Megner, Linda
AU - Christensen, Ole Martin
AU - Rouse, Jordan
AU - Kim, Dae Wook
N1 - Funding Information:
Acknowledgment. This work was a collaborative research work with the Wyant College of Optical Sciences for its assistance with the linear-astigmatism-free, three-mirror system development. This research was made possible in part by the Technology Research Initiative Fund Optics/Imaging Program at the University of Arizona.
Funding Information:
Swedish National Space Agency; National Research Council of Science and Technology (CAP-15-01-KBSI). This work was a collaborative research work with the Wyant College of Optical Sciences for its assistance with the linear-astigmatism-free, three-mirror system development. This research was made possible in part by the Technology Research Initiative Fund Optics/Imaging Program at the University of Arizona.
Publisher Copyright:
© 2020 Optical Society of America
PY - 2020/6/10
Y1 - 2020/6/10
N2 - We present optical characterization, calibration, and performance tests of the Mesospheric Airglow/Aerosol Tomography Spectroscopy (MATS) satellite, which for the first time, to the best of our knowledge, for a satellite, applies a linear-astigmatism-free confocal off-axis reflective optical design. Mechanical tolerances of the telescope were investigated using Monte Carlo methods and single-element perturbations. The sensitivity analysis results indicate that tilt errors of the tertiary mirror and a surface RMS error of the secondary mirror mainly degrade optical performance. From the Monte Carlo simulation, the tolerance limits were calculated to ±0.5 mm, ±1 mm, and ±0.15◦ for decenter, despace, and tilt, respectively. We performed characterization measurements and optical tests with the flight model of the satellite. Multi-channel relative pointing, total optical system throughput, and distortion of each channel were characterized for end-users. Optical performance was evaluated by measuring the modulation transfer function (MTF) and point spread function (PSF). The final MTF performance was 0.25 MTF at 20 lp/mm for the ultraviolet channel (304.5 nm), and 0.25-0.54 MTF at 10 lp/mm for infrared channels. The salient fact of the PSF measurement of this system is that there is no noticeable linear astigmatism detected over a wide field of view (5.67◦ × 0.91◦). All things considered, the design method showed great advantages in wide field of view observations with satellite-level optical performance.
AB - We present optical characterization, calibration, and performance tests of the Mesospheric Airglow/Aerosol Tomography Spectroscopy (MATS) satellite, which for the first time, to the best of our knowledge, for a satellite, applies a linear-astigmatism-free confocal off-axis reflective optical design. Mechanical tolerances of the telescope were investigated using Monte Carlo methods and single-element perturbations. The sensitivity analysis results indicate that tilt errors of the tertiary mirror and a surface RMS error of the secondary mirror mainly degrade optical performance. From the Monte Carlo simulation, the tolerance limits were calculated to ±0.5 mm, ±1 mm, and ±0.15◦ for decenter, despace, and tilt, respectively. We performed characterization measurements and optical tests with the flight model of the satellite. Multi-channel relative pointing, total optical system throughput, and distortion of each channel were characterized for end-users. Optical performance was evaluated by measuring the modulation transfer function (MTF) and point spread function (PSF). The final MTF performance was 0.25 MTF at 20 lp/mm for the ultraviolet channel (304.5 nm), and 0.25-0.54 MTF at 10 lp/mm for infrared channels. The salient fact of the PSF measurement of this system is that there is no noticeable linear astigmatism detected over a wide field of view (5.67◦ × 0.91◦). All things considered, the design method showed great advantages in wide field of view observations with satellite-level optical performance.
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U2 - 10.1364/AO.392187
DO - 10.1364/AO.392187
M3 - Article
C2 - 32543559
AN - SCOPUS:85086504888
SN - 1559-128X
VL - 59
SP - 5335
EP - 5342
JO - Applied optics
JF - Applied optics
IS - 17
ER -