Author Topic: Starship hot staging  (Read 483700 times)

Offline Eka

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Re: Starship hot staging
« Reply #1360 on: 11/14/2024 08:14 am »
Long term thoughts on hot staging and hot staging ring integration into booster.

Right now Starship has 3 vacuum Raptors, but that is eventually going to be 6. With three vacuum Raptors things don't balance out nicely for exhaust during staging separation. All must be fired, and exhaust from one or two will blow hard on the grid fin hardware and of its protection. With 6, 2 could be initially fired for hot staging and have lots of space for exhaust to escape. The grid fin hardware can stay above the dome. Putting it inside the tank is a PITA. For this I'm aligning the two that are fired 90 degrees to the vertical plane through the catch pins. This centers them in the area between the grid fin hardware. They now have plenty of space for exhaust to escape.

Exhaust vents will be as much as possible all the way around. For aesthetics reasons I don't expect to see a triangulated tube system, or we'd already have it.

I suspect COPVs, guidance computers and other hardware tucked in at the top of the tank will be moved to the tops of the chines. Less vibrations during hot staging. Some could be tucked under the grid fin hardware, but that space is at a premium for grid fin actuator hardware and supports. It may also require grid fin hardware removal for its maintenance.

Even for 3 vacuum raptor Starships, I expect the hot staging top for the booster will migrate to what I described above. The grid fin hardware protection shields must be able to handle 3+ engine hot staging fires if there is failure to light either of the two initially fired engines.
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Offline Twark_Main

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Re: Starship hot staging
« Reply #1361 on: 11/14/2024 10:05 am »
Long term thoughts on hot staging and hot staging ring integration into booster.

Right now Starship has 3 vacuum Raptors, but that is eventually going to be 6. With three vacuum Raptors things don't balance out nicely for exhaust during staging separation. All must be fired, and exhaust from one or two will blow hard on the grid fin hardware and of its protection. With 6, 2 could be initially fired for hot staging and have lots of space for exhaust to escape. The grid fin hardware can stay above the dome. Putting it inside the tank is a PITA. For this I'm aligning the two that are fired 90 degrees to the vertical plane through the catch pins. This centers them in the area between the grid fin hardware. They now have plenty of space for exhaust to escape.

[me] likes this.

Exhaust vents will be as much as possible all the way around. For aesthetics reasons I don't expect to see a triangulated tube system, or we'd already have it.

Errr, see attached....

It's so odd to me that one would consider triangulated tubes to be unaesthetic.  The current assembly method essentially makes tubes, but with an inefficient round-about manufacturing method. The "tube diameter" [sic] is smaller, so you need more tubes, so both cost and flow resistance goes up.

The resulting ad-hoc "tubes" aren't circular, whereas real circular tubes are cheaper. So again both cost and flow resistance goes up.

For me, that makes the current (interim) design quite un-aesthetic. I look at it and I don't see clean lines or snazzy silhouettes, I just see poor (ie not yet done) design. This must be what Elon Musk means when he says "When I look at something, I don't see what's right, I can only see what's wrong with the design. This is not a recipe for happiness."   :-\

Offline KilroySmith

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Re: Starship hot staging
« Reply #1362 on: 11/14/2024 03:39 pm »
That image seems to show the grid fin motors moving into the upper tank - at the very least, they're mounted significantly lower than on the current boosters.
And it shows the upper dome sticking ABOVE the walls of the booster. 
« Last Edit: 11/14/2024 03:40 pm by KilroySmith »

Offline Twark_Main

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Re: Starship hot staging
« Reply #1363 on: 11/14/2024 04:09 pm »
That image seems to show the grid fin motors moving into the upper tank - at the very least, they're mounted significantly lower than on the current boosters.
And it shows the upper dome sticking ABOVE the walls of the booster.

Pointing out mistakes (if any) is just a distraction from the fact that the graphics designer was definitely instructed to replace the existing hot staging ring with a tube truss design.  Unless your theory is that their pen slipped? Or they were told to just make up the entire thing willy-nilly with zero instructions given?

For aesthetic and functional reasons I expect to see a triangulated tube system (plus, otherwise the illustration wouldn't have it).


Physics says it's better. Manufacturability says it's better. Cost says it's better. Mass says it's better. And SpaceX has tipped their hand that this is their ultimate plan. On the counter-argument side, all we have is...  what again?   One guy doesn't like the look?
« Last Edit: 11/14/2024 04:52 pm by Twark_Main »

Offline Slarty1080

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Re: Starship hot staging
« Reply #1364 on: 11/14/2024 05:39 pm »
Long term thoughts on hot staging and hot staging ring integration into booster.

Right now Starship has 3 vacuum Raptors, but that is eventually going to be 6. With three vacuum Raptors things don't balance out nicely for exhaust during staging separation. All must be fired, and exhaust from one or two will blow hard on the grid fin hardware and of its protection. With 6, 2 could be initially fired for hot staging and have lots of space for exhaust to escape. The grid fin hardware can stay above the dome. Putting it inside the tank is a PITA. For this I'm aligning the two that are fired 90 degrees to the vertical plane through the catch pins. This centers them in the area between the grid fin hardware. They now have plenty of space for exhaust to escape.

Exhaust vents will be as much as possible all the way around. For aesthetics reasons I don't expect to see a triangulated tube system, or we'd already have it.

I suspect COPVs, guidance computers and other hardware tucked in at the top of the tank will be moved to the tops of the chines. Less vibrations during hot staging. Some could be tucked under the grid fin hardware, but that space is at a premium for grid fin actuator hardware and supports. It may also require grid fin hardware removal for its maintenance.

Even for 3 vacuum raptor Starships, I expect the hot staging top for the booster will migrate to what I described above. The grid fin hardware protection shields must be able to handle 3+ engine hot staging fires if there is failure to light either of the two initially fired engines.
Are two engines sufficient to pull a fully tanked Starship away from a mostly depleted Superheavy with engines running?
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Offline r8ix

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Re: Starship hot staging
« Reply #1365 on: 11/14/2024 05:44 pm »
Long term thoughts on hot staging and hot staging ring integration into booster.

Right now Starship has 3 vacuum Raptors, but that is eventually going to be 6. With three vacuum Raptors things don't balance out nicely for exhaust during staging separation. All must be fired, and exhaust from one or two will blow hard on the grid fin hardware and of its protection. With 6, 2 could be initially fired for hot staging and have lots of space for exhaust to escape. The grid fin hardware can stay above the dome. Putting it inside the tank is a PITA. For this I'm aligning the two that are fired 90 degrees to the vertical plane through the catch pins. This centers them in the area between the grid fin hardware. They now have plenty of space for exhaust to escape.

Exhaust vents will be as much as possible all the way around. For aesthetics reasons I don't expect to see a triangulated tube system, or we'd already have it.

I suspect COPVs, guidance computers and other hardware tucked in at the top of the tank will be moved to the tops of the chines. Less vibrations during hot staging. Some could be tucked under the grid fin hardware, but that space is at a premium for grid fin actuator hardware and supports. It may also require grid fin hardware removal for its maintenance.

Even for 3 vacuum raptor Starships, I expect the hot staging top for the booster will migrate to what I described above. The grid fin hardware protection shields must be able to handle 3+ engine hot staging fires if there is failure to light either of the two initially fired engines.
Are two engines sufficient to pull a fully tanked Starship away from a mostly depleted Superheavy with engines running?

Presumably, it would still involve the 3 SL engines, so 5 instead of 6 or 9...

Offline KilroySmith

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Re: Starship hot staging
« Reply #1366 on: 11/14/2024 06:15 pm »
That image seems to show the grid fin motors moving into the upper tank - at the very least, they're mounted significantly lower than on the current boosters.
And it shows the upper dome sticking ABOVE the walls of the booster.

Pointing out mistakes (if any) is just a distraction from the fact that the graphics designer was definitely instructed to replace the existing hot staging ring with a tube truss design.  Unless your theory is that their pen slipped? Or they were told to just make up the entire thing willy-nilly with zero instructions given?

For aesthetic and functional reasons I expect to see a triangulated tube system (plus, otherwise the illustration wouldn't have it).


Physics says it's better. Manufacturability says it's better. Cost says it's better. Mass says it's better. And SpaceX has tipped their hand that this is their ultimate plan. On the counter-argument side, all we have is...  what again?   One guy doesn't like the look?

Sorry about that; I didn't mean to take exception to your points at all; in fact, I fully agree with you.
The graphic definitely shows a tube interstage, just pointing out that it also shows the grid fins getting moved below the upper dome, which has been a topic of conversation as to whether that would happen or not.  Frankly, what it shows is an extremely clean implementation of a permanently attached HSR, and I like the tube structure, the lowered grid fins and naked dome.

Offline rsdavis9

Re: Starship hot staging
« Reply #1367 on: 11/24/2024 05:25 pm »
I thought(perhaps mistakenly) that they had a control problem with the grid fins with the HSR still attached and thats why they jettisoned it? Something to do with supersonic flow interacting with the booster body.
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Offline StraumliBlight

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Re: Starship hot staging
« Reply #1368 on: 08/07/2025 12:04 pm »
A couple of interesting slides from a NASA presentation last year.

SpaceX Starship Hot Staging - From Concept to Flight [Nov 16, 2024]

Quote
To analyze Starship�s hot staging maneuver, researchers in the Fluid Dynamics Branch at NASA�s Marshall Space Flight Center performed computational fluid dynamics (CFD) simulations using the Loci/CHEM flow solver. These simulations included steady-state simulations as well as sophisticated time-accurate moving body simulations on a variety of iterations of the Starship geometry. Due to the scale of the problem, meshes of approximately 500 million cells were required. The team simulated various engine startup sequences and analyzed the resulting aerodynamic loads. Flight data from Starship�s second Integrated Flight Test (IFT2) compared favorably to the CFD results. These simulations supported SpaceX in designing a successful hot-staging separation.

NASA SC24 Hot Staging

Offline equiserre

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Re: Starship hot staging
« Reply #1369 on: 08/07/2025 02:11 pm »
Very interesting!
What peak pressures are reached in that shield and in the interstage space in general? have any numbers (order of mag) been published?

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