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Fly to the moon question-2



Hi AMSATs,

I see that with an ion-engine it is possible to go
from a GTO into lunar orbit. This is very
interresting, because then I only have one more
question:

What we need to get from this lunar orbit save to the
lunar surface ??? How much Newton thrust for how much
radio weight is needed ? I guess a ion-engine will
have not enough thrust, or not ??

Kind regards,
73 de PE1RAH, William
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