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Development of the Laser Altimeter (LIDAR) for Hayabusa2

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Abstract

Hayabusa2 was launched on 3 December 2014 on an H-IIA launch vehicle from the Tanegashima Space Center, and is, at the time of writing, cruising toward asteroid 162137 Ryugu (\(1999\mathrm{JU}_{3}\)). After reaching the asteroid, it will stay for about 1.5 years to observe the asteroid and collect surface material samples.

The light detection and ranging (LIDAR) laser altimeter on Hayabusa2 has a wide dynamic range, from 25 km to 30 m, because the LIDAR is used as a navigation sensor for rendezvous, approach, and touchdown procedures. Since it was designed for use in planetary explorers, its weight is a low 3.5 kg. The LIDAR can serve not only as a navigation sensor, but also as observation equipment for estimating the asteroid’s topography, gravity and surface reflectivity (albedo). Since Hayabusa2 had a development schedule of just three years from the start of the project to launch, minimizing development time was a particular concern. A key to shortening the development period of Hayabusa2’s LIDAR system was heritage technology from Hayabusa’s LIDAR and the SELENE lunar explorer’s LALT laser altimeter.

Given that the main role of Hayabusa2’s LIDAR is to serve as a navigation sensor, we discuss its development from an engineering viewpoint. However, detailed information about instrument development and test results is also important for scientific analysis of LIDAR data and for future laser altimetry in lunar and planetary exploration. Here we describe lessons learned from the Hayabusa LIDAR, as well as Hayabusa2’s hardware, new technologies and system designs based on it, and flight model evaluation results. The monolithic laser used in the laser module is a characteristic technology of this LIDAR. It was developed to solve issues with low-temperature storage that were problematic when developing the LIDAR system for the first Hayabusa mission. The new module not only solves such problems but also improves reliability and miniaturization by reducing the number of parts.

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Authors and Affiliations

  1. Japan Aerospace Exploration Agency, 3-1-1 Yoshinodai Chuo-ku, Sagamihara, Kanagawa, 252-5210, Japan

    T. Mizuno, M. Mita, F. Terui & Y. Mimasu

  2. Department of Space and Astronautical Science, School of Physical Sciences, Japan Aerospace Exploration Agency, SOKENDAI (The Graduate University for Advanced Studies), 3-1-1 Yoshinodai Chuo-ku, Sagamihara, Kanagawa, 252-5210, Japan

    T. Mizuno

  3. NEC Corporation, 1-10 Nisshin-cho, Fuchu, Tokyo, 183-8501, Japan

    T. Kase & T. Shiina

  4. National Astronomical Observatory of Japan, 2-2-1 Osawa, Mitaka, Tokyo, 181-8588, Japan

    N. Namiki, R. Yamada & H. Noda

  5. Planetary Exploration Research Center, Chiba Institute of Technology, 2-17-1 Tsudanuma, Narashino, Chiba, 275-0016, Japan

    H. Senshu

  6. National Institute of Information and Communications Technology, 4-2-1 Nukui-kitamachi, Koganei, Tokyo, 184-8795, Japan

    H. Kunimori

  7. Research Center for Advanced Information Science and Technology, University of Aizu, Aizu-wakamatsu, Fukushima, 965-8580, Japan

    N. Hirata

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  1. T. Mizuno
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  2. T. Kase
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  3. T. Shiina
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  4. M. Mita
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  5. N. Namiki
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  6. H. Senshu
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  7. R. Yamada
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  8. H. Noda
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  9. H. Kunimori
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  10. N. Hirata
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  11. F. Terui
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  12. Y. Mimasu
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Corresponding author

Correspondence to T. Mizuno.

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Mizuno, T., Kase, T., Shiina, T. et al. Development of the Laser Altimeter (LIDAR) for Hayabusa2. Space Sci Rev 208, 33–47 (2017). https://doi.org/10.1007/s11214-015-0231-2

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  • DOI: https://doi.org/10.1007/s11214-015-0231-2

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