• DocumentCode
    3207780
  • Title

    Developing an efficient Space System Rapid Design Center

  • Author

    Reynerson, Charles M.

  • Author_Institution
    Ball Aerosp. & Technol. Corp., Boulder, CO, USA
  • Volume
    7
  • fYear
    2001
  • fDate
    2001
  • Firstpage
    7
  • Abstract
    A Space System Rapid Design Center (RDC) can be used in quickly sizing and estimating the cost of space systems. Given candidate mission requirements for a satellite or constellation, clean-sheet of paper designs can be formulated resulting in the definition of key system parameters, such as size, power, weight, and payload performance. Rough cost models (Unmanned Spacecraft Cost Model - USCM, Small Satellite Cost Model - SSCM) can be linked to this to assist in determining Life Cycle Cost estimates. Existing spacecraft buses can be compared to the clean-sheet of paper design to determine their suitability for a particular mission. Higher fidelity tools can be used to link the spacecraft design to the mission data to assess impacts on mission effectiveness. Comparing the capabilities of a RDC to that of traditional aerospace concept design team processes, vehicle designs and performance information can be produced with a fraction of the resources and in much less time
  • Keywords
    design engineering; life cycle costing; space vehicles; Space System Rapid Design Center; aerospace design; life cycle costing; small satellite cost model; spacecraft design; unmanned spacecraft cost model; vehicle design; Aerospace industry; Costs; Government; Payloads; Power system modeling; Process design; Proposals; Satellites; Space technology; Space vehicles;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2001, IEEE Proceedings.
  • Conference_Location
    Big Sky, MT
  • Print_ISBN
    0-7803-6599-2
  • Type

    conf

  • DOI
    10.1109/AERO.2001.931429
  • Filename
    931429