Does anyone have any objective criteria (either from publications or technical reports) detailing what typical +Gz loads and durations are for current manned space craft (Orion, Dragon, Starship for example) during take off and orbital re-entry? I am trying to determine an appropriate +Gz Cut-Off. For the Space-Shuttle, I have read it was about +2.5 Gz, but could not find an exact duration of this load. At minimal, I would need a source saying what the expected +Gz load would be for a manned crew for current space craft.

Thanks in advance.

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