Ongoing electronic component miniaturization

AOC Number

41

Primary domain

T

Secondary domain

Description

Miniaturization of electronic systems is often an enabling factor for demanding aerospace missions. This is also true for avionics elements, where miniaturization often goes hand in hand with a reduction of power consumption which permits achieving further mass savings.

Potential hazards

  1. Susceptibility of line replaceable units to ionizing radiation as a result of ongoing component miniaturization
  2. Inadequate power and cooling needs
  3. Inadequate physical separation of miniaturized systems

Corroborating sources and comments

http://spacewire.esa.int/edp-page/papers/Avionics%20Architectures%20and%20Components%20for%20Planetary%20Entry%20Probes%20-%20Session%20V%20-%20Trautner%20-%20V1.0.pdf

Radiation testing campaign for a new miniaturized space GPS receiver,
Underwood, C.; Unwin, M.; Sorensen, R.H.; Frydland, A.; Jameson, P.;
Surrey Space Centre, Surrey Univ., Guildford, UK, Radiation Effects Data Workshop, 2004 IEEE

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