testAlphaIIIStructure
Three fins in finset, so Ixx and Iyy are reduced by a factor of 3
Ixx reduced from 5.2771946530250825E-5 to 1.7590648843416942E-5
Iyy reduced from 1.3580770106050167E-4 to 4.526923368683389E-5
Total rocket MOI changed to Ir=1.8763734635622462E-5 and
It=2.1238394331365588E-4
testFalcon9HComponentMOI
Three fins in finset, so
finset rotational MOI changed from 0.00413298 to 0.001377661595723823
finset longitudinal MOI changed from 0.01215133 to 0.004050443797127646
testFalcon9HeavyBoosterLaunchMOIs
Two finsets, each three fins. Each finset's MOI are reduced as in
testFalcon9HComponentMOI, resulting in change to totals
Ir=0.013480523485489424, It=0.07017476021288252
testFalcon9HeavyBoosterSpentMOIs
Two finsets, each three fins, as above
Ir=0.010420016485489425, It=0.06398514917026163
testFalcon9HeavyBoosterStageMassOverride
Two finsets, each three fins, as above
Ir=0.007100144485489424, It=16.030625168315694
testFalcon9HeavyComponentCMxOverride
Two finsets, each three fins, as above
Ir=0.007100144485489424, It=0.047289449862727435
testFalcon9HeavyComponentMassOverride
Two finsets, each three fins, as above
Ir=0.026027963480146098, It=0.35928666329363634
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