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how do i calculate the thrust of the rocket , its exit velocity and Specific impulse from just its mass flow rate? I have data about the gas i.e. xenon, and its mass flow rate at exit.
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As we know about NEXT ion thruster developed by NASA and simulate thrusters by different organizations, they have a common design technique- a bombardment region which releases ions for thrust (...
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Which free available simulation software is there which could help simulate ion path after they are released from a source under action of magnetic and electric and other fields and depending on...
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