An ocean reentry was always statistically the most likely. It appears China won its gamble (unless we get news of debris in the Maldives). But it was still reckless
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I do see more than one people pointed out the drop zone issue for this type of LEO mission in Wenchang. Some claims doing sub-orbit would result the core stage hitting south Europe/Middle East. I am not familiar with this thats why I am asking different opinion on this issue.
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It depends on the exact cutoff velocity. An optimal sub-orbit might hit S Europe, but you can choose a slightly less than optimal one that will hit the Atlantic safely.
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I do not think orbits are the issue. The YF-77s on LM-5B core are not restartable, so any de-orbit engines are extra weight.
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I think the major problem here is that each module will have to make their first burn right after payload separation, w/o solar panel. The CSS is using flexible panels with a very complicated deployment schedule (~30mins for the two arrays on Tianhe).
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And I am worrying about the robustness of this trajectory as the rocket has no way to make any correction after engine shutdown. In fact, CASC mentioned that directed orbital insertion is one of the key challenges they solved during the development of this rocket.
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As from journal articles, the acceleration of the rocket will be ~3.0G at MECO, and the residual thrust will last ~5.5s after the commanded shutdown. If the timing is off, it might lead to huge trouble...
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