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General Discussion / Re: Starship!
« Last post by bknight on May 28, 2023, 09:43:32 AM »I would like some of our "rocket scientists" here have a look at this video and offer their opinions. It is an animated render and commentary giving a brief explanation of how the water-cooled steel plate system is supposed to work. Its from Alpha Tech's YouTube channel, with the computer rendering by Ryan Hansen. Credit to both of them for this excellent presentation.
Note: right-click on the link and choose to play it in a new tab. It will play a short (1m 41s) video in Dropbox
https://www.dropbox.com/s/1zi550dn801f41m/Starship%20Deluge.mp4?raw=1
As most of you already know, I am an aeronautical engineer (retired), but not an aerospace engineer. While the two disciplines share a lot of common ground, there are aspects of "rocket science" that are outside my pay-grade.
In particular, there are some statements made that I am doubting the accuracy of. I would appreciate any comments on some of these technical details.
1. The claimed "established temperature gradient" between the rocket exhaust at the point it leaves the ending bells and the water cooled plate
2. "In the centre of the plate, the water pressure is higher than the exhaust pressure"
3. "The exhaust never touches the plate"
4. If the water flow is maintained at a high enough rate, they can keep the temperature at the plate below 1000°C
5. In the real world, the plate never sees more than a couple of hundred degrees C
I'm not an aerospace engineer either but have some experience with high flow water rates/pressures.
It seems to me that 2,3,4 are dictated by a high enough rate to prove all the cases correct. Since I don't know the temperature of the exhaust nor the profile of the exhaust i can't peak of those parameters. I suspect they have either modelled or calculated the exhaust from engine bell to tip of exhaust, so they know the temperature/pressure regime that the water flow will experience and then back calculate how much flow is needed to offset the exhaust. I don't know the diameter of the holes nor the number of the holes, but this two would be a somewhat easy calculation in fluid flow requirements.