• DocumentCode
    2688283
  • Title

    MIDEX advanced modular and distributed spacecraft avionics architecture

  • Author

    Ruffa, John A. ; Castell, Karen ; Flatley, Thomas ; Lin, Michael

  • Author_Institution
    NASA Goddard Space Flight Center, Greenbelt, MD, USA
  • Volume
    5
  • fYear
    1998
  • fDate
    21-28 Mar 1998
  • Firstpage
    531
  • Abstract
    MIDEX (Medium Class Explorer) is the newest line in NASA´s Explorer spacecraft development program. As part of the MIDEX charter, the MIDEX spacecraft development team has developed a new modular, distributed, and scaleable spacecraft architecture that pioneers new spaceflight technologies and implementation approaches, all designed to reduce overall spacecraft cost while increasing overall functional capability. This resultant “plug and play” system dramatically decreases the complexity and duration of spacecraft integration and test, providing a basic framework that supports spacecraft modularity and scalability for missions of varying size and complexity. Together, these subsystems form a modular, flexible avionics suite that can be modified and expanded to support low-end and very high-end mission requirements with a minimum of redesign, as well as allowing a smooth, continuous infusion of new technologies as they are developed without redesigning the system. This overall approach has the net benefit of allowing a greater portion of the overall mission budget to be allocated to mission science instead of a spacecraft bus. The MIDEX scaleable architecture is currently being manufactured and tested for use on the Microwave Anisotropy Probe (MAP), an in-house program at GSFC
  • Keywords
    avionics; modules; redundancy; space vehicle electronics; space vehicles; Explorer spacecraft development program; MIDEX; Medium Class Explorer; Microwave Anisotropy Probe; NASA; flexible avionics suite; functional capability; overall mission budget; overall spacecraft cost; scalability; scaleable spacecraft architecture; spacecraft avionics architecture; spacecraft modularity; spaceflight technologies; Aerospace electronics; Aircraft manufacture; Anisotropic magnetoresistance; Cost function; Manufacturing; Probes; Scalability; Space technology; Space vehicles; System testing;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 1998 IEEE
  • Conference_Location
    Snowmass at Aspen, CO
  • ISSN
    1095-323X
  • Print_ISBN
    0-7803-4311-5
  • Type

    conf

  • DOI
    10.1109/AERO.1998.685863
  • Filename
    685863