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
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