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The most serious thing is that the angular design of the propulsion of the shuttle is not compensated by the center of gravity of the launcher, this causes an extremely slow and dangerous ascent rate of about 10º. Also, assuming that you pass the barrier of 5000, which is the most dangerous stage, when uncoupling the solid fuel engines, the ejector system makes them hit with the wings of the shuttle, causing reentry to be impossible. Thanks and best regards.