Welcome to Tesla Motors Club
Discuss Tesla's Model S, Model 3, Model X, Model Y, Cybertruck, Roadster and More.
Register

SpaceX Starship - Integrated Flight Test #2 - Starbase TX - Including Post Launch Dissection

This site may earn commission on affiliate links.
is reentry on headers?
I can't see how else they'd start the engines. I'm envisioning that restart, burn, shutdown, flip, then reentry, lots of deceleration and heating that affects the propellants in the header tanks. If the header feed lines are on the tile side then the descent angle should ensure that the remaining propellants in the header tanks should want to fill the feed lines (eliminating any voids). With all that reentry heating, they have an easy way to pressurize the tanks.

Hmmm. The orbital flip should be done such that the header tanks should again want to push remaining propellant into the feed lines. That would be a flip away from the tile side.

Just some blue sky thoughts.
 
Why not vent your simulated payload - LOX - after reaching orbit and after shutting Starship engines off, during coasting period?
Full credit to @mongo
The velocity vs propellant use was off due to less mass, so they were venting to match the values expected during reentry. Since it's autogenously pressurized they had to do this while the engines were running.
 
  • Like
Reactions: Electroman
So... if the Ship RUD was due to LOX bleed-off in order to lose mass, it would seem a very easy fix... mass simulator being the obvious one.

But... assuming that a normal ship would have had both LOX and cargo, doesn't that imply it was lighter than would be typically expected anyway?

If so, then it would seem that some of our earlier speculation about ship thrust impacting and affecting the booster may not be as manageable with reducing ship thrust, as it may need it for separation...
 
So... if the Ship RUD was due to LOX bleed-off in order to lose mass, it would seem a very easy fix... mass simulator being the obvious one.

But... assuming that a normal ship would have had both LOX and cargo, doesn't that imply it was lighter than would be typically expected anyway?

If so, then it would seem that some of our earlier speculation about ship thrust impacting and affecting the booster may not be as manageable with reducing ship thrust, as it may need it for separation...
Ship + propellant is 1300 tons
With payload is 1400 tons, only 8% more
So fairly minimal impact at separation
 
  • Like
Reactions: scaesare
If so, then it would seem that some of our earlier speculation about ship thrust impacting and affecting the booster may not be as manageable with reducing ship thrust, as it may need it for separation...
Fooey. My speculation was to double booster thrust. Keep the energies at staging as high as possible without breaking anything. I think SpaceX was just emphatic about that second bit for their first hot staging attempt.
 
My only thought is that SpaceX didn't want any other angles of staging shown through the government site. One of those trade secret things. I was really looking forward to seeing the WB-57 angle of staging and boostback, so going to REDACTED was pretty disappointing.
Ahh, you're thinking SpaceX didn't want to show it... I was thinking maybe the Gov't didn't for some reason ...
 
  • Like
Reactions: JB47394
Here's each video at full resolution, starting with the WB-57 footage. Folks in the comments point out that the Starship lost a lot of tiles. You can see "lines" and "dots" of white appear on the Starship as it rises, showing the underlayment. By the 45 second mark, it's pretty obvious. I guess that's why SpaceX is going with the smaller tiles; they give more attachment points per surface area.

 
  • Like
Reactions: scaesare
Here's each video at full resolution, starting with the WB-57 footage. Folks in the comments point out that the Starship lost a lot of tiles. You can see "lines" and "dots" of white appear on the Starship as it rises, showing the underlayment. By the 45 second mark, it's pretty obvious. I guess that's why SpaceX is going with the smaller tiles; they give more attachment points per surface area.

Still not hot staging :(

Tiles and insulating materials seem to be the bane of launch vehicles. Funny how something so seemingly simple is such an issue...
 
  • Like
Reactions: JB47394
Tiles and insulating materials seem to be the bane of launch vehicles. Funny how something so seemingly simple is such an issue...
I think these launches are MUCH more violent then people can appreciate. Unless you have been fortunate enough to attend a launch up close and personal (or actually ridden in one !!) it is hard to appreciate the forces involved.
 
I think these launches are MUCH more violent then people can appreciate. Unless you have been fortunate enough to attend a launch up close and personal (or actually ridden in one !!) it is hard to appreciate the forces involved.
Ther shockwaves in some of the videos attest to that, but I suspect you are right and no way to really appreciate not in person... would love to see a launch live.
 
  • Like
Reactions: ICUDoc
I think these launches are MUCH more violent then people can appreciate.
Nah. Liquid propellant rockets give a very smooth ride. Shuttle astronauts invariably comment on how different the ride is before and after staging the SRBs.

Here's a statement by Akihiko Hoshide to Kyoto News about his ride in a Dragon capsule:
The launch and landing itself it's just like another spacecraft, but it was smooth, I think it was more responsive that's what's I remember going up hill, you know the acceleration and deceleration, that was like, it was like a joyride. I still remember that day when up all four of us were whoop, yayy just cheering and giggling all the way until MECO [Main Engine Cutoff]

For vehicles with more engines, I expect an even smoother ride because a glitch in one engine has a smaller overall effect. At an extreme, if one engine instantly shut down, you'd only lose 3% of your thrust. I wonder if the astronauts would even notice. Do that on Falcon 9 and you lose 11%. Saturn V and you lose 20%.

I attribute the loss of tiles to aerodynamic forces. Each barrel section has its tiles applied by machine, and the alignment of the tile surfaces is very uniform. The hand-installed tiles that fill in all the gaps are much less uniform. I assume air gets in there and tears them off.
 
  • Like
Reactions: petit_bateau
Folks in the comments point out that the Starship lost a lot of tiles.
I’m a bit stunned by the number of lost tiles revealed in that video. The TPS team must be under tremendous pressure to figure out a solution.

Speaking only for myself, I’m not riding Starship to LEO until there have been multiple missions with ZERO lost tiles! :p
 
I’m a bit stunned by the number of lost tiles revealed in that video. The TPS team must be under tremendous pressure to figure out a solution.
Once there is a gap it gets harder to keep them on.
Super Done vs hurricane...

Speaking only for myself, I’m not riding Starship to LEO until there have been multiple missions with ZERO lost tiles! :p
Well, it depends how you're getting back from LEO. 😉