
From the early Apollo Command Service Module (CSM) instrument panel, January 1966.
Its function was to gauge propellants feeding the CSM main engine (SPS) and also allowed the crew to assume manual control of propellant feed rates.
Mouse over the photo for details from the Apollo Operations Handbook, November 12, 1966.
All of these knobs, and manual overrides, backup shunts, and display and sensor test features achieve one goal – to keep the flow rate of the two propellant fluids in a 2:1 ratio for the SPS rocket engine.
It was pulled out of a warehouse IVO Edwards AFB (apparently made its way from NASA via DRMO surplus facility there).
Location of this subpanel in the overall Block I instrument panel, with the 



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