And to make it even faster

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Found it!
It should be sin(a) / (v / 8 - cos(a) / 2).
Dsekercioglu (talk)17:15, 24 September 2017

The only correct formula to calculate the escape angle of orbital movement where <math>v_{retreat}</math> is not zero is using integral.

Anything else is wrong.

Xor (talk)17:18, 24 September 2017