• DocumentCode
    2769709
  • Title

    Team Xc: JPL´s collaborative design team for exploring CubeSat, NanoSat, and SmallSat-based mission concepts

  • Author

    Zarifian, Pez ; Imken, Travis ; Matousek, Steve E. ; Moeller, Robert C. ; Bennett, Matthew W. ; Norton, Charles D. ; Rosenberg, Leigh ; Alibay, Farah ; Spangelo, Sara ; Banazadeh, Payam ; Casillas, Raul Polit ; Kawata, Jessie

  • Author_Institution
    Jet Propulsion Lab., Pasadena, CA, USA
  • fYear
    2015
  • fDate
    7-14 March 2015
  • Firstpage
    1
  • Lastpage
    10
  • Abstract
    Recently there has been an increasing demand for a rapid mission concept generation capability for CubeSats, NanoSats, and SmallSats at JPL and in the broader community in the Concept Maturity Level (CML) 2-5 range. To help address these needs, JPL´s Innovation Foundry has extended its long-standing advanced concepts concurrent engineering team, Team X, with a new, agile, and collaborative design capability called Team Xc. This concurrent team-based approach provides rapid turnaround for small spacecraft mission and system early concept studies. The process is adaptable to a wide variety of CubeSat, NanoSat, and SmallSat customers and mission applications. Team Xc design and analysis services include feasibility assessments, trade space exploration studies, and point design studies, commensurate with the level of maturity of the mission concept. The team is assembled with experts experienced in designing, building, launching, and operating CubeSats; leaders in mission architecture, spacecraft design, and concurrent engineering methods; and subject matter experts tailored to the specific needs of each study and customer. The Team Xc capability has been applied to several studies and extended to cover a large breadth of missions spanning applications including Earth science, planetary science, astrophysics, and technology demonstration. Team Xc draws from Team X, JPL, and external subject matter experts to produce quick-turnaround reports targeted to each customer´s needs.
  • Keywords
    artificial satellites; CML 2-5 range; CubeSat; Earth science; JPL collaborative design team; NanoSat; SmallSat-based mission concepts; Team Xc analysis services; Team Xc design; astrophysics; collaborative design capability; concept maturity level; concurrent engineering methods; concurrent team-based approach; mission architecture; planetary science; small spacecraft mission; spacecraft design; technology demonstration; Mars; Propulsion; Solid modeling; Space exploration; Space vehicles; Three-dimensional displays;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2015 IEEE
  • Conference_Location
    Big Sky, MT
  • Print_ISBN
    978-1-4799-5379-0
  • Type

    conf

  • DOI
    10.1109/AERO.2015.7119221
  • Filename
    7119221