• DocumentCode
    2434236
  • Title

    Structural Bus and Release Mechanisms on the ST5 Satellites - Summary and Status

  • Author

    Rossoni, Peter

  • Author_Institution
    NASA Goddard Space Flight Center, Greenbelt
  • fYear
    2007
  • fDate
    3-10 March 2007
  • Firstpage
    1
  • Lastpage
    14
  • Abstract
    The Space Technology 5 Mechanical System met the challenge of packaging a fully functional science and technology satellite system with its Deployer mechanism into a compact 0.07 m3 volume. Three 25 kg satellites were orbited in constellation in March, 2006. The ST5 mechanical system is composed of (1) The Structural Bus; (2) Magnetometer Instrument Boom (3) Spacecraft Deployer Release Mechanism. This system includes a highly integrated electronics enclosure as a multifunctional structure; a lightweight, magnetically clean Magnetometer Boom; the first use of Nitinol Shape-Memory Alloy trigger devices for deploying multiple spacecraft; an innovative compliant mount for the umbilical connector and a Deployer mechanism that imparts both separation velocity and mission spin rate to three constellation flying satellites. These elements employed cutting-edge design and analysis tools, state-of-the-art testing facilities and proven engineering techniques to meet stringent performance criteria, enabling the mission´s success.
  • Keywords
    artificial satellites; Deployer mechanism; ST5 satellites; Space Technology 5 Mechanical System; magnetometer instrument boom; mass 25 kg; release mechanisms; structural bus; Aerospace electronics; Instruments; Magnetic devices; Magnetic separation; Magnetometers; Mechanical systems; Packaging; Satellites; Space technology; Space vehicles;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2007 IEEE
  • Conference_Location
    Big Sky, MT
  • ISSN
    1095-323X
  • Print_ISBN
    1-4244-0524-6
  • Electronic_ISBN
    1095-323X
  • Type

    conf

  • DOI
    10.1109/AERO.2007.352783
  • Filename
    4161318