Avionics technology challenges for lunar/Mars exploration

Details Avionics technology challenges for lunar/Mars exploration Avionics technology challenges for lunar/Mars exploration

Mar 1992

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1992aiaa.conft....h&link_type=abstract

AIAA, Space Programs and Technologies Conference, Huntsville, AL, Mar. 24-27, 1992. 9 p.

Computer Science

Architecture (Computers), Avionics, Lunar Exploration, Manned Mars Missions, Space Exploration, Configuration Management, Radiation Protection, Spacecraft Shielding, Vibration Damping

Scientific paper

Avionics technology challenges for the lunar/Mars exploration infrastructure are discussed. Emphasis is placed on the architecture, the basic structure of the avionics system, including sensors and effectors; the environment, which determines conditions in which the avionics system must operate; and operations and logistics, including the ability to support and ensure avionics system availability. Open architecture concepts employing standard building blocks are considered to be promising, particularly when applied across the entire lunar/Mars infrastructure. The use of avionics module designs developed for aircraft programs will make it possible to control costs and increase flexibility and reliability, but it raises questions about tolerance to vibration, shock, radiation, and temperature.

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