Poll

Eventual Fate of SN4?

Boom, crumple or pop before even getting off the ground.
83 (14.5%)
Starts flight tests but ends up crashing gloriously.
302 (52.9%)
Completes flight tests proud and unscathed.
186 (32.6%)

Total Members Voted: 571

Voting closed: 04/21/2020 12:43 am


Author Topic: SpaceX Starship : Texas Prototype(s) Thread 8 : Discussion  (Read 401777 times)

Offline alang

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Is it plausible that they are spraying antifreeze to avoid ice formation during cryo tests?



Doubt it, it's not gonna stick on the surface for too long, especially once they start cryo testing. Water's going to condense on the surface. If it doesn't freeze, it's going to bead up and run off, taking the anti freeze with it. After a short time, ice is going to form anyways in that case.

In very cold conditions, when they spray anti freeze on airplanes, the plane needs to take off quickly after application because it's gonna freeze up if they wait too long without reapplying it.

Could there be a need to test the effect of icing in different external humidity conditions and this is a cheap way to do it?

Offline DusanC

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Having a large number of intricate tile shapes might not be a problem by itself as long as they don't require a manual repairs. Unlike on the Shuttle there is no chance of getting hit by debris during launch.

For tiling a rounded cone they could do it using the same slightly warped hexagon at each height point.

But they might eventually go for unique shapes of varying thickness anyway in order to optimize mass.

It's actually mathematically impossible to tile a rounded cone with any sort of uniform warped hexagon.  If you try it, you'll find that it works alright at the beginning, but as the surface continues curving, your hexagons will become more and more distorted until you're forced to add pentagons to the mix.  This is a direct consequence of the Euler Identity.

There's just no way to avoid requiring a large number of different tile shapes when trying to tile a surface with non-zero curvature.  (A cylinder has, mathematically speaking, zero curvature, just to be clear on this.  Not so for a rounded cone)

Mathematically you're correct.

But engineers like to cheat ;D

1 type of tile in 2 forms, whole and cut in half.

PS: I'd like to emphasize that only 200deg of SS needs to be tiled.

Does that work the same on a stronger curvature near the tip of the nose cone or will the vertical distance between the rows of half tiles be lower than 1 row?
Limits of this "cheat" are defined by:
1. Size of tile
2. Allowed variation of gap between tiles.

So smaller tiles with larger gap can cover stronger curvature (smaller radius)

I'd need those 2 dimensions to say what's that radius but I presume with this cheat more than 95% of surface can be tiled, even more if we introduce  cutting of tiles with waterjet to different widths to cover corner cases.

To solve the problem of stronger curvatures I would introduce  2nd tile of the same type but smaller so that 3 small tiles can be placed on side of 1 larger tile

PS. Correction, 3 tiles on side.

PPS. Added sketch

For more tile robustness and to increase allowed tile gap variation I would use stepped tiles so that tiles overlap, like scales or roof tiles.

Offline Phantom

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I understand that the fewer the number of unique tiles the better, but aren't there some compelling issues requiring at least a small number of distinct tiles?

1-The problem of the shape of the rocket is obvious.

2-As I understand from comments in this thread the heat problem at the nose is greater than it is for the rest of the vehicle.  Big gaps may not be appropriate.  Maybe there needs to be a thicker, or a different type of insulator for this area.

I wonder if a reasonable solution might be to use at least four types of tiles:  hexagons and half-hexes similar to the ones being tested on SN4, plus a "cap" and a small number of "isosceles trapezoid" tiles that extend from the cap to the regular, cylindrical part of the ship.  Again, these latter tiles might be thicker or somehow more heat resistant than the hexes.

Offline Johnnyhinbos

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Can the tile discussion please be brought over to the starship engineering thread?
John Hanzl. Author, action / adventure www.johnhanzl.com

Online Herb Schaltegger

Guys, can you please take the mathematical discussions of tile geometry to the General Engineering thread and leave this thread to the discussion of what’s actually happening with the specific prototypes now being built and tested?
Ad astra per aspirin ...

Offline rakaydos

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Or even a separate thread for heat shield tiling. Mods?

Offline capoman

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Pretty sure all that spraying last night was likely something simple as soap for a leak check. Not sure if they would do this as part of the room temperature N2 test anyway, or they detected a pressure drop and then decided to do the test. Thing is, a very small leak on such a large vessel would be hard to detect by measurement in a short time, so I wouldn’t be surprised if this would be a standard procedure going forward with any new tank.

Online Chris Bergin

Or even a separate thread for heat shield tiling. Mods?

Feel free to set up a new thread (always room for splinter threads in this section), then return to this thread with the link so everyone knows where to go. :) Anyone can start a new thread and perhaps open it by quoting some of the best tile posts from this thread as part of an opening summary. That'd work!
« Last Edit: 04/26/2020 12:59 pm by Chris Bergin »
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Offline Observation

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I think we have seen the spray test on Mk1 but not on the others. Not sure if that means thst they're being extra cautious with this one.

Offline Slothman

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Pretty sure all that spraying last night was likely something simple as soap for a leak check. Not sure if they would do this as part of the room temperature N2 test anyway, or they detected a pressure drop and then decided to do the test. Thing is, a very small leak on such a large vessel would be hard to detect by measurement in a short time, so I wouldn’t be surprised if this would be a standard procedure going forward with any new tank.

I thought about it and I'm not sure if they would really apply soapy water with a high pressure sprayer. I think they would spray it locally in small quantities on the welds. It literally only takes a thimble full of soapy water on a leak spot to bubble up. No need to douse the surrounding sheet metal.
And from the scale of things (cloud compared to 9m tank diameter), they really applied heavy quantities of whatever it was at a high pressure (large cloud of very fine mist, it seemed).

It just doesn't make sense to apply soapy water like that if they have to closely observe the welds to spot any bubbling anyways, so they should apply it in a more conservative manner.

That.. or they just don't care. Who knows  ;D

Offline testguy

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Is it plausible that they are spraying antifreeze to avoid ice formation during cryo tests?


More likely a soap solution looking for bubbles.  I would assume they depressurized to a safe level first.  It does not look to me to be a concentrated spray at high pressure. 
« Last Edit: 04/26/2020 03:49 pm by testguy »

Offline Wolfram66

Is it plausible that they are spraying antifreeze to avoid ice formation during cryo tests?


More likely a soap solution looking for bubbles.  I would assume they depressurized to a safe level first.  It does not look to me to be a concentrated spray at high pressure.

They are probably applying the same hydrophobic material with which they coat the F9 cores. Works well for Falcon.

Offline Norm38

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What does “ambient pressure test” mean?

Offline RoboGoofers

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What does “ambient pressure test” mean?
ambient temp, I assume.

Offline RonaldRaygun

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What does “ambient pressure test” mean?

I am assuming he misspoke slightly and meant to say ambient temperature pressure test. Both because that's been the sequence in the past and is how he referred to that test previously, and because SN4 was venting fairly energetically which would have been impossible at ambient pressure.

Just differentiating between last night's gaseous N2 test and later liquid N2 tests at cryo temperatures (and even higher pressures than last night.)

Offline GregTheGrumpy

I expect the GN2 was fairly cold when they pumped it in.  I saw the top and bottom frost over fairly quickly and all over (not bottom up).  Then the frosting starting going away and the vending shortly after (if memory serves correctly).

Would it be correct to guess that raising the cold GN2 to ambient would induce a nice even pressure gradient suitable for finding small leaks?

What do they use for leak detection?  I note the spraying but they moved so fast and at large quantity that I'm thinking that was really a hydrophobic coating more than a soap bubble test. Yes?  No?

Offline awests

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I expect the GN2 was fairly cold when they pumped it in.  I saw the top and bottom frost over fairly quickly and all over (not bottom up).  Then the frosting starting going away and the vending shortly after (if memory serves correctly).

Would it be correct to guess that raising the cold GN2 to ambient would induce a nice even pressure gradient suitable for finding small leaks?

What do they use for leak detection?  I note the spraying but they moved so fast and at large quantity that I'm thinking that was really a hydrophobic coating more than a soap bubble test. Yes?  No?

I would assume the GN2 is sourced from the big LN2 tank on the farm, either they pull from the headspace of the tank or they run the LN2 through an expansion. In either case, the GN2 will probably go through a heat exchanger to bring the GN2 up to "ambient" temperature. I do not remember SN4 tanks frosting over until after venting. The only sign of the GN2 test was smoothing of the dents, as pointed out by someone on the LabPadre stream.

Most likely they were spraying soapy water rather than some sort of coating or antifreeze.

Online Spock1108

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Most likely they were spraying soapy water rather than some sort of coating or antifreeze.

Ok, but why spray water and soap AFTER the pressure test? ???
Francesco Maio

Offline Keldor

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Most likely they were spraying soapy water rather than some sort of coating or antifreeze.

Ok, but why spray water and soap AFTER the pressure test? ???

Maybe an initial high pressure test to verify structural integrity?  After that, if it held up to 5 bar or whatnot, you can be pretty confident that it's safe to approach at 0.1 bar for bubble leak tests.

Offline cdebuhr

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I expect the GN2 was fairly cold when they pumped it in.  I saw the top and bottom frost over fairly quickly and all over (not bottom up).  Then the frosting starting going away and the vending shortly after (if memory serves correctly).

Would it be correct to guess that raising the cold GN2 to ambient would induce a nice even pressure gradient suitable for finding small leaks?

What do they use for leak detection?  I note the spraying but they moved so fast and at large quantity that I'm thinking that was really a hydrophobic coating more than a soap bubble test. Yes?  No?

I would assume the GN2 is sourced from the big LN2 tank on the farm, either they pull from the headspace of the tank or they run the LN2 through an expansion. In either case, the GN2 will probably go through a heat exchanger to bring the GN2 up to "ambient" temperature. I do not remember SN4 tanks frosting over until after venting. The only sign of the GN2 test was smoothing of the dents, as pointed out by someone on the LabPadre stream.

Most likely they were spraying soapy water rather than some sort of coating or antifreeze.
Emphasis mine.  When you want large volumes of gas (and you're not making it yourself onsite with, e.g., an air fractionation plant), you have two options. 1) Get large volumes of compressed gas delivered (tube trailers), or 2) get liquid delivered and run it through a gassifier (generally just a big air-warmed heat exchanger).  There's several gassifiers around the build site attached to the larger liquid argon tanks (see BocaChicaGal pic below).  They must go through boatloads of argon gas TIG welding.  There's also a big one at the launch site.  Its tucked in the gap between two of the three vertical black cryotanks at the LOX (? - what I'm the LOX farm is the  tank cluster closer to the road) farm.  See drone pic posted recently by Elon Musk.

The smaller "lab sized" LAr dewars you see all over the site also have gassifiers, they're just not visible externally.  They're typically in the form of tubing soldered or brazed to the inner wall of the outer vacuum jacket of the dewar.

Edit: In case it wasn't obvious enough from the text above ... Image credit: (1) BocaChicaGal; (2) Elon Musk & Co.
« Last Edit: 04/26/2020 06:56 pm by cdebuhr »

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