• DocumentCode
    381622
  • Title

    Integration and test for small shuttle payloads

  • Author

    Wright, Michael R.

  • Author_Institution
    Dept. Flight Syst. Integration & Test, NASA Goddard Space Flight Center, Greenbelt, MD, USA
  • Volume
    1
  • fYear
    2002
  • fDate
    2002
  • Abstract
    Recommended approaches for small space shuttle payload integration and test (I&T) are presented. The paper is intended for consideration by developers of small shuttle payloads, including I&T managers, project managers, and system engineers. Examples and lessons learned are presented based on the extensive history of NASA\´s Hitchhiker project. All aspects of I&T are presented, including: I&T team responsibilities, coordination, and communication; flight hardware handling practices; documentation and configuration management; I&T considerations for payload development; I&T at the development facility; prelaunch operations, transfer, orbiter integration and interface testing; and postflight operations. This paper is of special interest to those payload projects that have small budgets and few resources: that is, the truly "faster, cheaper, better" projects. All shuttle small payload developers are strongly encouraged to apply these guidelines during I&T planning and ground operations to take full advantage of today\´s limited resources and to help ensure mission success.
  • Keywords
    aerospace testing; configuration management; space vehicles; system documentation; Hitchhiker project; communication; configuration management; coordination; development facility; documentation; flight hardware handling practices; ground operations; interface testing; orbiter integration; payload development; payload integration and test; small shuttle payloads; team responsibilities; Aerospace engineering; Document handling; Engineering management; Hardware; History; Payloads; Project management; Space shuttles; Systems engineering and theory; Testing;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference Proceedings, 2002. IEEE
  • Print_ISBN
    0-7803-7231-X
  • Type

    conf

  • DOI
    10.1109/AERO.2002.1036834
  • Filename
    1036834