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  1. I'm thinking about diving deeper into the ion engines of KSP. Not only can I understand them better for KSP fanworks, in which the engine math would be described in great detail, but I can apply these principles for real-life. As a KSP example, the given values of the IX-6315 "Dawn" engine are: Isp = 4200 s Thrust = 2 kN Which is way higher than the real-life ion engines I've been seeing. Values I can easily calculate are: Mass flow rate for xenon propellant (kg/s) Exhaust velocity (m/s) Beam power (watts) Wet-to-dry mass r
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