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Using air density profiles for Kerbin, there should be a way to find the most fuel-efficient trajectory for launch. This could definitely be done numerically, or by the calculus of variations. Other options are possible.
The text was updated successfully, but these errors were encountered:
Using air density profiles for Kerbin, there should be a way to find the most fuel-efficient trajectory for launch. This could definitely be done numerically, or by the calculus of variations. Other options are possible.
The text was updated successfully, but these errors were encountered: