
This Valve Package Assembly (VPA) is a Q4 1965 prototype of the control valves for the ascent engine of the Apollo Lunar Module (RS-18).
I can see now why Neil Armstrong had nightmares about this specific system.
It’s a wildly complex design compared to all of the other hypergolic bipropellant motors I have from Apollo (R-4D, SE-8, LMDE) and Gemini (SE-6). The VPA was a mission critical assembly; had the solenoid valves failed to open and supply propellant to the Ascent Engine, there was no getting home.
Neil’s nightmare was that at the completion of the mission, he pushes the button, and nothing happens. It’s a setup for a sequence of tough decisions. Do you go for a long walk?
Some historical notes from spaceaholic: Notice the fuel ducting on the left appears larger and more bulbous then its companion oxidizer line. During testing of the Ascent engine, pre-ignition pressure spikes were observed; this was resolved by lengthening the path the fuel had to take so that timing of its arrival at the injector was delayed to occur until slightly after the oxidizer (the ducting wraps back on itself to extend the path length).











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