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(Partial answer) I noticed between the info in the question, additional info in comments, and an assumption of 0.0 delta thrust at 0.0 flowrate, there was enough information to draw a exponential curve for the throttle. Delta Thrust (N) Inert Prop Flowrate (kg/s) 0 0 4146140 4.18 10141140 20.0 13956140 37.6 Using this throttle characteristic curve, I ...


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