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Re:SLS vs. Starship by m4rtink on Friday November 13, 2020 @11:54PM (#25090393)
>All liquid rocket engines are reusable. As always there are exceptions - rs-68 has an ablative nozzle that is rated for a single flight, so you need to test without that I guess.

Other engines could be similarly rated for jinutes of runtime by default for maximum performance. SpaceX aldo repeatedly ststed Merlin and Raptor were designed for cheap and fregvent reuse.

Re:SLS vs. Starship by pfdietz on Saturday November 14, 2020 @07:49AM (#25092006)
Yes, Merlin was designed to be cheap. That's why it's cheap. Being reusable was not an impediment to it being cheap. Being reusable is not an excuse for being expensive.

A cheap rocket engine needs a cheap development process, which means you want your test articles to last a long time. Far from being an obstacle to cheapness, reusability is a requirement for an affordable engine development program.

Let's go way back to Usenet and listen to Henry Spencer on this subject.

https://yarchive.net/space/rocket/rl10.html

"To reiterate my original point: almost any regeneratively-cooled liquid rocket engine is reusable, even if it was built for expendable vehicles. The design requirement for the F-1 was 20 starts and 2250s of firing; as part of the test program, six of them accumulated over 5000s each."