The bump of Why can't you just parachute down from orbit? got me curious about if hypersonic parachutes were even a thing, but before I found out I stumbled back across LOFTID, which apparently had a successful test. However, a cursory glance at the literature makes it seem like all the proposed applications for inflatable decelerators like LOFTID are for Mars entry (aside from something like the old Paracone), despite the tests being at Earth.
Is there some really clear trade-off/trade-stufy that makes inflatable decelerators not attractive for reentry from LEO versus other options? Something else like TRL too low? Am I just wrong?
I saw Does an inflatable heat shield have some capacity to be used for LEO Earth's atmospheric entry? and GremlinWranger's answer makes some relevant claims but I'm imagining there's some clearer existing consensus about what re-entry scenarios inflatable heat shields are useful for (maybe parameterized by payload weight vs energy?).