It's mostly something I thought about myself. The prompting idea was how to massively reduce the capex of a turbine system, even if that increases the marginal cost per kWh when the system is in use, and also the observation of th incredibly high power density of rockets (they're the highest power density heat engines humanity makes). So, get rid of the compressor stage of the turbine, be open cycle so there's no need to condense steam back to water, and operate at higher pressure (at least an order of magnitude higher than combustion turbines) so the entire thing can be smaller.

You'd have to pay for storage of water and LOX (and making the LOX) so this wouldn't make sense to prolonged usage. On the plus side, using pure LOX means no NOx formation, so you also lose the catalytic NOx destruction system a stationary gas turbine would need to treat its exhaust.

I vaguely recall some people in Germany were looking at something like this but I don't remember any details.