H7142
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Everything posted by H7142
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O now ofc thrust profiles are usually more complex then just one value: Original sources
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Is there some kind of equation that is used to calculate the loft angle, there are equations that can determine this angle.
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So has this finalized the move to the new missile aero FM? I saw mentions of things like motor on drag reductions in the previous thread and was wondering if those have been modeled now are will take more time.
