Earlier quoted context omitted.
SpaceX Starship is way outside established industry specifications.
How so?
Every production rocket is fully expendable. Launch, expect discard of 100%* of launch system. Starship is designed for 100% reusable, with same-day fly/land/refuel/repeat. That’s obviously a huge difference.
* - exceptions:
Space Shuttle discarded most of the launch system, acting as glider to return crew/cargo and some engines. Reuse turnaround was months, with extensive repairs expected. Boosters required prolonged recovery and refurbishing, with high likelihood of loss.
Falcon 9 is only one remotely viable for same day return to pad and reuse of first stage. Second stage is discarded.
SN# is a fast-reuse second stage. Landing involves leveraging the terminal velocity physics of a brick (not gentle glide of Shuttle), followed by effectively flipping a 16-story building ~90° in free fall with powered deceleration to 0m/s in less than 2km vertical.
Nothing in the industry resembles the fast launch/fall/relight/reorientate/decelerate/land/refuel/repeat sequence, of SN#. There is no established industry specifications addressing such operation. And as the history of rocketry shows, establishing such specifications practically involves lots of crashes. [cue How Not To Land A Booster]