n72.75
Seize the means of computation
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I am trying to do an off plant transfer to the moon from an equatorial low earth orbit.
I can change the TEj and TIn until i get the minimal dV but it will take a lot of time and a lot of gesswork.
What I want to know is if there is any method of finding minimal dV eject windows (less then 3.75km/s).
I can change the TEj and TIn until i get the minimal dV but it will take a lot of time and a lot of gesswork.
What I want to know is if there is any method of finding minimal dV eject windows (less then 3.75km/s).