1,360
edits
Space Shuttle Avionics: Difference between revisions
Jump to navigation
Jump to search
→FUEL CELLS (DISP 69)
| Line 200: | Line 200: | ||
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 === | |||
[[File:Shuttle avionics DISP67.jpg|600px|ELECTRIC display of the Space Shuttle]] | |||
On this display, information on the power consumption and distribution throughout the Shuttle can be found. It shows the voltages measured at the main DC and AC buses as well as the current flowing through the systems and the total consumption of all systems aboard the orbiter. | |||
Almost all data displayed (except the detailed distribution across the forward, mid and aft distribution assemblies) is meaningful and reflects the systems running aboard the Shuttle as well as the position of the bus connector and tie switches. | |||
=== FUEL CELLS (DISP 69) === | === FUEL CELLS (DISP 69) === | ||