nhnifong Posted September 12, 2012 Share Posted September 12, 2012 Since in KSP drag equation uses mass instead of area, more fuel (0.2 drag coeff.) would give me bigger drag losses...So what is the drag on a part? mass * coeff_of_drag * atmo_density ?There's no benefit to using aerodynamics at all? What about wings, the orientation obviously matters for those, so does it matter for all parts?What's the equation for lift?Anybody know these equations?(not the real ones, the ones in KSP's code) Link to comment Share on other sites More sharing options...
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