I think 5000 psi as maximum should already be enough range. It allows enough thermal expension, is below the proof pressure of regulator and tank and should still be able to indicate a failed overpressure vent valve.Ok. I will make that 7500 psi gauge and use the get Propellant value and have 10.4 be 100% which is 5000 psi, correct
Do we need that cutoff handle?
I don't know if temperature can be measured in Orbiter? So I will use the get Propellant value and have 10.4 be 100% which is 5000 psi, correct
Maybe the green at 4500 psi +/- 5% for predeployment pressure check?