• DocumentCode
    2788779
  • Title

    Approach for on-orbit maintenance and experiment plan using 150kg-class satellites

  • Author

    Kimura, Shinichi ; Nagai, Yasufumi ; Yamamoto, Hiroshi ; Masuda, Kazumi ; Abe, Naohiko

  • Author_Institution
    Nat. Inst. of Inf. & Commun. Technol., Tokyo
  • fYear
    2005
  • fDate
    5-12 March 2005
  • Firstpage
    837
  • Lastpage
    845
  • Abstract
    With the maturation of space technology, there is an increasing focus on the maintenance of space craft and the space environment. NICT (National Institute of Information and Communications Technology) has proposed an Orbital Maintenance System (OMS), which is a rescue-and-removal satellite-servicing system for telecommunications satellites, and has conducted research on related technologies. One of the biggest challenges in on-orbit maintenance is the development of autonomous rendezvous technologies. The rescue satellite must be able to approach the target satellite before it falls out of orbit. Meanwhile NICT and Mitsubishi Heavy Industries (MHI) have been planning a unique small-satellite mission called SmartSat-1. Using SmartSat-1, NICT and MHI are planning to carry out experiments on autonomous rendezvous technologies for the OMS. In this paper, we describe the next demonstration mission for the orbital maintenance system, which will utilize the 150-kg class twin-sat, SmartSat-1
  • Keywords
    artificial satellites; maintenance engineering; 150 kg; Mitsubishi Heavy Industries; National Institute of Information and Communications Technology; Orbital Maintenance System; SmartSat-1 satellite; rescue satellites; telecommunications satellites; Aerospace industry; Artificial satellites; Communication industry; Communications technology; Humans; Orbital robotics; Space debris; Space technology; Technology planning; Telescopes;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2005 IEEE
  • Conference_Location
    Big Sky, MT
  • Print_ISBN
    0-7803-8870-4
  • Type

    conf

  • DOI
    10.1109/AERO.2005.1559375
  • Filename
    1559375