• DocumentCode
    2553051
  • Title

    Spacecraft modular architecture design for on-orbit servicing

  • Author

    Reynerson, Charles M.

  • Author_Institution
    Ball Aerosp. & Technol. Corp., Boulder, CO, USA
  • Volume
    4
  • fYear
    2000
  • fDate
    2000
  • Firstpage
    227
  • Abstract
    The Spacecraft Modular Architecture Design (SMAD) Concept involves the use of an on-orbit servicing vehicle to replace and/or replenish components on a spacecraft. This study was conducted to evaluate the potential cost and benefits for on-orbit satellite servicing. Actual satellite data were used to estimate a baseline cost and to establish an operational design. This paper gives an overview of the study including the selection of servicing methodology, benefits of servicing, spacecraft impacts, selection of spacecraft components/subsystems to service, derived servicer requirements, servicer point design, and a costing evaluation
  • Keywords
    artificial satellites; cost-benefit analysis; life cycle costing; maintenance engineering; baseline cost; components selection; on-orbit servicing; operational design; potential cost-benefits; rendezvous docking; satellite servicing; servicer point design; servicer requirements; servicing methodology; servicing vehicle; spacecraft modular architecture design; Costing; Costs; History; Low earth orbit satellites; Orbital robotics; Payloads; Space shuttles; Space stations; Space technology; Space vehicles;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference Proceedings, 2000 IEEE
  • Conference_Location
    Big Sky, MT
  • ISSN
    1095-323X
  • Print_ISBN
    0-7803-5846-5
  • Type

    conf

  • DOI
    10.1109/AERO.2000.878426
  • Filename
    878426