Electric Propulsion Sizing
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Thrust
152.96 mN
0.15296 N
Propellant mass
25.268 kg
30.0 day burn
Total impulse
396,465.7 N s
Ve 15,691 m/s
Mass flow
9.748 mg/s
propellant throughput
Electric thrust chain
153.0 mN
Input power becomes jet power; exhaust velocity then trades thrust against propellant flow.
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