I have 3D printed a 1/50 scale Saturn V and now I'm modeling it in Rocksim to calculate how much nose weight will be needed to make it stable. When I look at the Rocksim file provided by Apogee for their 1/70 scale Saturn V, I see that they have taken the profile of the F-1 fairings and created fins that are basically 2 dimensional outlines of a 3 dimensional object. If I do the same thing on my model, I end up needing 2 lbs. of nose weight to get at least 1 caliber of stability on the motor combinations that I'm interested in. Fine.
On the other hand, if I create pods containing conical nosecones and use them as the fairings, I end up needing 3 lbs. of nose weight to get the same stability. Does it makes sense that half a cone imparts less stability than a fin of the same cross section? How does Apogee get away with doing it that way, is the Saturn V short/fat enough to benefit from base drag? Is there something else I could be missing?
On the other hand, if I create pods containing conical nosecones and use them as the fairings, I end up needing 3 lbs. of nose weight to get the same stability. Does it makes sense that half a cone imparts less stability than a fin of the same cross section? How does Apogee get away with doing it that way, is the Saturn V short/fat enough to benefit from base drag? Is there something else I could be missing?