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Space Shuttle Avionics: Difference between revisions
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→SM APU/HYD (DISP 86)
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On this display, a summary of various pressure and temperature readings of the APU and hydraulics systems can be accessed. All parameters are meaningful and represent the internal state of the simulation and possible failure modes. | On this display, a summary of various pressure and temperature readings of the APU and hydraulics systems can be accessed. All parameters are meaningful and represent the internal state of the simulation and possible failure modes. | ||
=== SM PL RET (DISP97) === | |||
[[File:Shuttle avionics pl ret.jpg|600px|PL RET display (DISP 97) of the Space Shuttle]] | |||
The payload retention display is used to monitor the status of the payload retention system latch microswitches. It indicates the current latch status as well as whether a payload is in the correct position to be latched. | |||
Currently only the payload position 1 is functional, the others are not yet implemented in FG. | |||