an example from the F-4E
the commonly cited maximum thrust is ~17,000 lbs per engine which roughly corresponds to sea level static uninstalled thrust
while the actual maximum installed thrust is over 23,000 lbs per engine
the commonly cited maximum thrust is ~17,000 lbs per engine which roughly corresponds to sea level static uninstalled thrust
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there are graphs showing this for the F100 but idk if i can show these. they arent from military afaik but still
yeah idk on those
this is from a report in ~1970 about installing wing slats
so its definitely safe