• DocumentCode
    3200771
  • Title

    Asteroid surface probes: A low-cost approach for the in situ exploration of small solar system objects

  • Author

    Cottingham, Christopher M. ; Deininger, William D. ; Dissly, Richard W. ; Epstein, Kenneth W. ; Waller, David M. ; Scheeres, Daniel J.

  • Author_Institution
    Ball Aerosp.&Technol. Corp., Boulder, CO
  • fYear
    2009
  • fDate
    7-14 March 2009
  • Firstpage
    1
  • Lastpage
    11
  • Abstract
    In-situ characterization of the surface properties of small solar system objects, such as asteroids and comets, is important to understanding their properties and evolution. Ball Aerospace & Technologies Corp.´s asteroid surface probes (ASP) provide a vehicle to gather specific in-situ scientific data that cannot be obtained from orbiting craft. A simple architecture with a small form factor, taking advantage of miniaturized, shock-resistant electronics and sensors, allows these probes to accommodate a variety of scientific instrumentation in softball to basketball-sized packages. The small size enables the probes to be deployed as additional payloads on host spacecraft, rather than requiring dedicated missions. This paper discusses the system concept and architecture of Ball´s ASPs, benefits of their size and simplicity, unique scientific data available from in-situ measurements, and the flexibility of multiple configuration/instrumentation options. We also discuss ongoing development work and near-term plans to increase the TRL level of many of the associated technologies.
  • Keywords
    asteroids; astronomical instruments; comets; asteroid surface probes; comets; orbiting craft; small solar system objects; Aerospace electronics; Application specific processors; Electronics packaging; Extraterrestrial measurements; Instruments; Payloads; Probes; Size measurement; Solar system; Space vehicles;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace conference, 2009 IEEE
  • Conference_Location
    Big Sky, MT
  • Print_ISBN
    978-1-4244-2621-8
  • Electronic_ISBN
    978-1-4244-2622-5
  • Type

    conf

  • DOI
    10.1109/AERO.2009.4839320
  • Filename
    4839320