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TGO

Posted 03-29-2016 at 03:32 PM by lzakelj

Quote:
Originally Posted by BrianJ View Post
Thanks Barry.


Hi,
yes, the launch is a challenge, there's not much (if any) dV to spare and the "Briz" 4th stage thrust is comparatively low, so the burns are long and you need them to be as efficient as possible. As far as I know, we don't have any trajectory planning utilities for Orbiter that can handle multiple-burn trajectory plans (possibly TransX can do that? Maybe a TransX expert can enlighten us).
So here's what I do for the Mars Transfer
...
Orbinaut
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