• DocumentCode
    381327
  • Title

    Integrated avionics system (IAS), integrating 3-D technology on a spacecraft panel

  • Author

    Hunter, Don I.

  • Author_Institution
    Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
  • Volume
    5
  • fYear
    2002
  • fDate
    2002
  • Firstpage
    2185
  • Abstract
    As spacecraft designs converge toward miniaturization, and with the volumetric and mass challenges placed on avionics, programs will continue to advance the "state of the art" in spacecraft system development with new challenges to reduce power, mass and volume. Traditionally, the trend is to focus on high-density component packaging technologies. Although new technologies have improved packaging densities, a system packaging architecture is required that not only reduces spacecraft volume and mass budgets, but increases integration efficiencies, provides modularity and flexibility to accommodate multiple missions while maintaining a low recurring cost. With these challenges in mind, a novel system packaging approach incorporates solutions that provide broader environmental applications and more flexible system interconnectivity. The integrated avionics system (IAS) provides for a low-mass, modular distributed or centralized packaging architecture which combines ridged-flex technologies, high-density COTS hardware and a new 3-D mechanical packaging approach, horizontal mounted cube (HMC). This paper will describe the fundamental elements of the IAS, HMC hardware design, system integration and environmental test results.
  • Keywords
    aerospace testing; avionics; environmental testing; packaging; space vehicle electronics; 3D technology; centralized packaging architecture; environmental applications; environmental test results; flexibility; flexible system interconnectivity; hardware design; high-density COTS hardware; high-density component packaging technologies; horizontal mounted cube; integrated avionics system; integration efficiencies; mechanical packaging approach; modularity; ridged-flex technologies; spacecraft designs; spacecraft panel; spacecraft system development; spacecraft volume; system packaging architecture; Aerospace electronics; Electronic packaging thermal management; Hardware; Packaging machines; Planets; Propulsion; Space missions; Space technology; Space vehicles; System testing;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference Proceedings, 2002. IEEE
  • Print_ISBN
    0-7803-7231-X
  • Type

    conf

  • DOI
    10.1109/AERO.2002.1035385
  • Filename
    1035385