5. In his derivation of Pdyn/Po, I think Bazant equates the design load capacity(mg) with his assumed mass of 58,000 tons (times g) for the upper part. I maintain there are two mgs one that should be used to establish the strain energy (mass1g) and one for design load capacity (mass2g). So the equation should really be:
Pdyn/Po = (1 + sqrt(1+2mass1gCh))/mass2g
6. Further, I believe 58,000 tons is overestimate for the mass of the upper part (mass1) by a factor of ~2.9 according to my work. His design load is also an underestimate of ultimare yield strength for the lower part. If I use my mass for the upper part and the 2.8 safety factor required by the code (refers to destructive testing of assemblies), I get Pdyn/Po of around 0.3 = no collapse. Don't forget, there is a sqrt on the upper part so it changes the ratio dramatically.
You need to go back and check your calculations, numbers, and formula. Keep in mind that all Pdyn/Po represents is the load magnification from impact. Altering the load above (i.e. lightening it) without modifying the stiffness (C) will actually result in greater load magnification (because you have a smaller object impacting a proportionally more rigid object). (Read Bazant's Addendum, he knows Po does not represent full load capacity.) Reducing the stiffness will result in less load magnification. However, there is a minimum stiffness required for the load above (which you can approximate as a lower bound). If you use dead load above only, select a reasonable ratio of dead load to live load, use the minimum stiffness of the floors immediately below only (i.e. assume that the entire tower structure from impact down to the ground is only as stiff as the columns at the impacted floor, a GROSSLY CONSERVATIVE assumption, because the tower is getting amazingly stiffer as you go down), you will still have an OVERLOAD, even with a FACTOR OF SAFETY.