• DocumentCode
    1747122
  • Title

    Implementation approach for Discovery-class missions

  • Author

    Vellinga, Joseph M.

  • Author_Institution
    Lockheed Martin Astronaut. Oper., Denver, CO, USA
  • Volume
    1
  • fYear
    2001
  • fDate
    2001
  • Firstpage
    42392
  • Abstract
    A sound implementation approach is necessary to win Discovery missions and is critical to successfully accomplishing the mission. The science concept is iterated with the design and implementation approach until a mission is defined that is within the 35-month development to launch period and the cost cap, and utilizes technology that permits implementation with acceptable program risk. The original mission concept must be defined in sufficient depth that development risks are low and the costs are well defined. This takes a very cooperative total team effort and willingness to be flexible to develop a balanced total mission package. Once selected the team must then commit to implement the mission within the agreement. This paper addresses the end-to-end implementation using Stardust, the fourth Discovery mission as a model. The author managed the industrial partner effort for Stardust development
  • Keywords
    aerospace computing; aerospace control; costing; planetary rovers; risk management; space research; space vehicles; Discovery-class missions; Stardust; acceptable program risk; balanced total mission package; comet samples; cooperative total team effort; cost cap; development risks; development to launch period; end-to-end implementation; implementation approach; return capsule; science requirements; software development; Costs; Earth; IEEE news; Laboratories; Mars; NASA; Packaging; Proposals; Space vehicles; Testing;
  • 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.2001.931692
  • Filename
    931692