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Space Shuttle Avionics: Difference between revisions
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→ELECTRIC
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In particular, it also allows to drive the opening sequence manually rather than automatically and has a software bypass implementation for the case of a failed main payload bay door switch. All functions of the original screen are implemented in FG. | In particular, it also allows to drive the opening sequence manually rather than automatically and has a software bypass implementation for the case of a failed main payload bay door switch. All functions of the original screen are implemented in FG. | ||
=== ELECTRIC === | === ELECTRIC (DISP 67) === | ||
[[File:Shuttle avionics DISP67.jpg|600px|ELECTRIC display of the Space Shuttle]] | [[File:Shuttle avionics DISP67.jpg|600px|ELECTRIC display of the Space Shuttle]] | ||