Earlier quoted context omitted.
> do rocket engines also have injectors Yes[1]. You want the fuel and oxidizer mixed as well as possible to achieve efficient combustion. There are also other small channels fuel has to flow through, like the ones used for regenerative cooling[2]. And not sure how well most turbopumps[3] would tolerate debris either, though that probably depends on the exact design. There are some really simple rocket designs out the…
I posted upthread, but another concern is that stray particulate is an ignition source. Rocket fuel pumps are ~100,000 hp, and that energy is put into kinetic energy of the fluid flow. A stray particulate can cause the metal pump and fuel lines to burn in the presence of O2 at 300 atmospheres.
That is wild. I need to learn more about rocket fuel pumps :-) Thank you all for these comments.