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学術論文

On-axis Optical Bench for Laser Ranging Instruments in future gravity missions

MPS-Authors

Yang,  Yichao
Laser Interferometry & Gravitational Wave Astronomy, AEI-Hannover, MPI for Gravitational Physics, Max Planck Society;

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Yamamoto,  Kohei
Laser Interferometry & Gravitational Wave Astronomy, AEI-Hannover, MPI for Gravitational Physics, Max Planck Society;

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Alvarez,  Dovale Miguel
Laser Interferometry & Gravitational Wave Astronomy, AEI-Hannover, MPI for Gravitational Physics, Max Planck Society;

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Delgado,  Juan Jose Esteban
Laser Interferometry & Gravitational Wave Astronomy, AEI-Hannover, MPI for Gravitational Physics, Max Planck Society;

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Müller,  Vitali
Laser Interferometry & Gravitational Wave Astronomy, AEI-Hannover, MPI for Gravitational Physics, Max Planck Society;

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Heinzel,  Gerhard
Laser Interferometry & Gravitational Wave Astronomy, AEI-Hannover, MPI for Gravitational Physics, Max Planck Society;

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フルテキスト (公開)

2202.00976.pdf
(プレプリント), 523KB

sensors-22-02070-v3.pdf
(出版社版), 555KB

付随資料 (公開)
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引用

Yang, Y., Yamamoto, K., Alvarez, D. M., Wei, D., Delgado, J. J. E., Müller, V., Jia, J., & Heinzel, G. (2022). On-axis Optical Bench for Laser Ranging Instruments in future gravity missions. Sensors, 22(5):. doi:10.3390/s22052070.


引用: https://hdl.handle.net/21.11116/0000-000A-30D5-F
要旨
The Laser Ranging Interferometer onboard the Gravity Recovery and Climate
Experiment Follow-On mission proved the feasibility of an interferometric
sensor for inter-satellite length tracking with sub-nanometer precision,
establishing an important milestone for space laser interferometry and the
general expectation that future gravity missions will employ heterodyne laser
interferometry for satellite-to-satellite ranging. In this paper we present the
design of an on-axis optical bench for next-generation laser ranging which
enhances the received optical power and the transmit beam divergence, enabling
longer interferometer arms and relaxing the optical power requirement of the
laser assembly. All design functionalities and requirements are verified by
means of computer simulations. A thermal analysis is carried out to investigate
the robustness of the proposed optical bench to the temperature fluctuations
found in orbit.