Hello, I am trying to use GMAT to simulate an interplanetary trajectory from LEO to Mars insertion using electric propulsion for future optimization. I would like to know more details on the polynomial used by GMAT for the electric thruster model. However, I cannot find any information concerning this in the User Guide or Mathematical Specifications document. Any information or resources you could point me to to help with this would be greatly appreciated.
Thank you for your time! Nick Goeckner
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