Author Topic: SpaceX Raptor LRE Proposed Successor: Project LEET-1337 LRE  (Read 104897 times)

Offline Hog

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Re: SpaceX Raptor LRE Proposed Successor: Project LEET-1337 LRE
« Reply #40 on: 09/20/2023 10:20 pm »
That sounds like a shockingly low number even for an expendable engine. Let’s say you have an engine acceptance test, a core stage acceptance test (like the green run), and then launch. That’s 3 of the four uses.

If you have to aborted lift-offs or green runs, you’d have to get new engines!

You can see why they deleted the green run even for crewed launches. They just don’t have the cycle life in the engines to afford that level of acceptance testing.

Just so very short-sighted.
My apologies, I attached the incorrect graphic, it's corrected now.  The Arty-1 through Arty-4 engines are the Adaptation engines with 6 starts.  The Restart engines come into usage for Artemis-5.
Your points still stand.
Paul

Offline Sarigolepas

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Re: SpaceX Raptor LRE Proposed Successor: Project LEET-1337 LRE
« Reply #41 on: 09/21/2023 03:09 pm »
Giving it a different name was likely just part of the internal politics of the time; a way for Musk to clearly distinguish between the initiative he felt was failing, and the one he felt was the way forwards. Once he sorted out the underlying problem there was no need for 2 different engine design tracks, so no need for 2 different names.
I think he is being serious about a new engine.

Offline Sarigolepas

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Re: SpaceX Raptor LRE Proposed Successor: Project LEET-1337 LRE
« Reply #42 on: 09/21/2023 03:22 pm »
Elon did make a statement a week or so ago about the Starship/Super heavy having the thrust of "three Saturn Vs".  Maybe he meant with this engine?  Even the proposed Raptor 3 thrust doesn't get you to three Saturn Vs.  Granted, maybe he didn't mean literally/exactly but it's still interesting he went from two at one point to three.
Do you have any source for that?
Also, 3 saturn V would be 320 tons of thrust per engine and more importantly a TWR of 1.8 at takeoff for an extended starship with a 6'000 tons gross weight. Such an high TWR makes sense if they make the second stage heavier relative to the first stage which would lead to lower velocity at MECO.

Offline Sarigolepas

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Re: SpaceX Raptor LRE Proposed Successor: Project LEET-1337 LRE
« Reply #43 on: 09/21/2023 03:33 pm »
If the price of Raptor is 1 million $, and we have no indication saying Musk was faking this number, it is already in a good spot (compared to other engines). But I know, he won't stop until they reach the limit.
In general I was surprised by the price of modern rocket engines compared to other complex machinery, like jet engines. The engines of the 737 MAX are 14.5 millions each. Sure the plane doesn't have 39 of them. But the price is comparable. Ofcourse  there are very big differences, but it isn't a totally out of the blue apples to oranges comparsion. I was initially surprised the prices were so close or maybe I was underestimating jet engine prices.
Jet engines are very complicated. Gas turbines can operate at over 1'600°C, each blade has regenerative and film cooling unlike raptor turbopumps which operate at 600°C
That's why I expect the LEET engine to have film cooling in the turbopumps. They are merging the fuel-rich turbopump with the injector so unless I'm mistaken they could extend the cooling channels from the combustion chamber all the way to the turbopumps.
They probably won't be able to reach 1'600°C thought because the pressure is higher than a gas turbine.

Offline steveleach

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Re: SpaceX Raptor LRE Proposed Successor: Project LEET-1337 LRE
« Reply #44 on: 09/21/2023 03:50 pm »
Giving it a different name was likely just part of the internal politics of the time; a way for Musk to clearly distinguish between the initiative he felt was failing, and the one he felt was the way forwards. Once he sorted out the underlying problem there was no need for 2 different engine design tracks, so no need for 2 different names.
I think he is being serious about a new engine.
A lot of things have changed since then, including new management for that division. He was probably serious about a new engine at the time, but he then found a different solution.

Offline Nomadd

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Re: SpaceX Raptor LRE Proposed Successor: Project LEET-1337 LRE
« Reply #45 on: 09/25/2023 06:23 am »
 Didn't the old, long life RS-25 need some pretty heavy refurbishment between launches?
 Maybe the low restart numbers for the single flight model is mostly from deleting the ability to overhaul it after every launch. Weld things that use to be bolted and such.
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Offline Sohl

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Re: SpaceX Raptor LRE Proposed Successor: Project LEET-1337 LRE
« Reply #46 on: 09/25/2023 02:43 pm »
Didn't the old, long life RS-25 need some pretty heavy refurbishment between launches?
 Maybe the low restart numbers for the single flight model is mostly from deleting the ability to overhaul it after every launch. Weld things that use to be bolted and such.

Seems reasonable and makes sense.  I don't have any particular knowledge of this, though.

Offline wannamoonbase

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Re: SpaceX Raptor LRE Proposed Successor: Project LEET-1337 LRE
« Reply #47 on: 09/25/2023 04:01 pm »
Didn't the old, long life RS-25 need some pretty heavy refurbishment between launches?
 Maybe the low restart numbers for the single flight model is mostly from deleting the ability to overhaul it after every launch. Weld things that use to be bolted and such.

I recall that the SSME was intended to go some number of flights between work, 4 or 8 flights, something like that.

But that after Challenger more is always better so they took them out and serviced them on each flight.

I don't know if it was warranted and if they found anything, or if it was a reflexive overreaction that stuck.

Seems that after 50+ years that we can do a lot better than the SSME, just on materials and manufacturing alone the RS-25 should be easy to improve on.  And not be $100M per engine.
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Offline Vahe231991

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Re: SpaceX Raptor LRE Proposed Successor: Project LEET-1337 LRE
« Reply #48 on: 09/25/2023 04:14 pm »
Giving it a different name was likely just part of the internal politics of the time; a way for Musk to clearly distinguish between the initiative he felt was failing, and the one he felt was the way forwards. Once he sorted out the underlying problem there was no need for 2 different engine design tracks, so no need for 2 different names.
I think he is being serious about a new engine.
Since the notional new engine is mentioned by Elon Musk as intended to help mankind become a multiplanetary species, I'm guessing that the Starship/Super Heavy would need to have the first stage modified to use as many as 12 engines with a total of 20 million pounds of thrust and the Starship portion fitted with five engines totaling 6 million pounds of thrust in order to burn enough fuel to reach portions of the solar system beyond Mars.

Offline ETurner

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Re: SpaceX Raptor LRE Proposed Successor: Project LEET-1337 LRE
« Reply #49 on: 09/25/2023 04:44 pm »
If the price of Raptor is 1 million $, and we have no indication saying Musk was faking this number, it is already in a good spot (compared to other engines). But I know, he won't stop until they reach the limit.
In general I was surprised by the price of modern rocket engines compared to other complex machinery, like jet engines. The engines of the 737 MAX are 14.5 millions each. Sure the plane doesn't have 39 of them. But the price is comparable. Ofcourse  there are very big differences, but it isn't a totally out of the blue apples to oranges comparsion. I was initially surprised the prices were so close or maybe I was underestimating jet engine prices.
Jet engines are very complicated. Gas turbines can operate at over 1'600°C, each blade has regenerative and film cooling unlike raptor turbopumps which operate at 600°C
That's why I expect the LEET engine to have film cooling in the turbopumps. They are merging the fuel-rich turbopump with the injector so unless I'm mistaken they could extend the cooling channels from the combustion chamber all the way to the turbopumps.
They probably won't be able to reach 1'600°C thought because the pressure is higher than a gas turbine.
Why would they want a turbine that operates at a much higher temperature? The combustion chamber is downstream.

Offline DJPledger

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Re: SpaceX Raptor LRE Proposed Successor: Project LEET-1337 LRE
« Reply #50 on: 09/25/2023 06:24 pm »
Giving it a different name was likely just part of the internal politics of the time; a way for Musk to clearly distinguish between the initiative he felt was failing, and the one he felt was the way forwards. Once he sorted out the underlying problem there was no need for 2 different engine design tracks, so no need for 2 different names.
I think he is being serious about a new engine.
Since the notional new engine is mentioned by Elon Musk as intended to help mankind become a multiplanetary species, I'm guessing that the Starship/Super Heavy would need to have the first stage modified to use as many as 12 engines with a total of 20 million pounds of thrust and the Starship portion fitted with five engines totaling 6 million pounds of thrust in order to burn enough fuel to reach portions of the solar system beyond Mars.
An F-1B thrust class next gen. engine would be perfect for a much larger next gen Starship system in the far future having the same engine counts for booster (33 engines) and ship (6 engines) as the current Starship system has.

Online Robotbeat

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Re: SpaceX Raptor LRE Proposed Successor: Project LEET-1337 LRE
« Reply #51 on: 09/26/2023 01:28 am »
Didn't the old, long life RS-25 need some pretty heavy refurbishment between launches?
 Maybe the low restart numbers for the single flight model is mostly from deleting the ability to overhaul it after every launch. Weld things that use to be bolted and such.

I recall that the SSME was intended to go some number of flights between work, 4 or 8 flights, something like that.

But that after Challenger more is always better so they took them out and serviced them on each flight.

I don't know if it was warranted and if they found anything, or if it was a reflexive overreaction that stuck.

Seems that after 50+ years that we can do a lot better than the SSME, just on materials and manufacturing alone the RS-25 should be easy to improve on.  And not be $100M per engine.
Why would the company making them want to charge less than $100 million per engine?
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Offline OTV Booster

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Re: SpaceX Raptor LRE Proposed Successor: Project LEET-1337 LRE
« Reply #52 on: 09/27/2023 05:01 pm »
A note about price.

If the price of Raptor is 1 million $, and we have no indication saying Musk was faking this number, it is already in a good spot (compared to other engines). But I know, he won't stop until they reach the limit.
In general I was surprised by the price of modern rocket engines compared to other complex machinery, like jet engines. The engines of the 737 MAX are 14.5 millions each. Sure the plane doesn't have 39 of them. But the price is comparable. Ofcourse  there are very big differences, but it isn't a totally out of the blue apples to oranges comparsion. I was initially surprised the prices were so close or maybe I was underestimating jet engine prices.

The BE4 engine costs about 8 milion, the RD180 25. The Merlin less than 1. The numbers are from EDA.

Those numbers are indeed crazy. But they aren't really comparable.

Elon always likes to talk about 'marginal cost' -- how much more it costs to make one additional engine. So the $1M figure doesn't include research and development, cost of the factory and equipment to build engines, profit, etc. No doubt if they were selling engines separately, the cost would be much higher.

Thanks for the explanation. This is indeed something I didn't consider. Hopefully raptor gets to the state of scaling that the marginal cost and the total ammortized price are nearly the same. IIUC what Elon says is useful if you want to make the design cheaper, but isn't good if you want to know the actual cost. He presumes they will get to the stage were R&D cost won't be vety significant.
Alberto, I'm just catching up on this thread.


Manufacturing and development costs are tricky and mushy so don't accept any of the numbers as you would an engineering number. For example, every hot fire of an installed engine and all launches to date can be considered engine development in some sense. To attribute the total cost of each hot fire or launch to engine development makes no sense but what proportion of costs should be apportioned to engine development?


Development costs could be ended when an engine leaves MacGregor but that doesn't make sense either. Until the engines are successfully integrated into a working system it can not be considered a finished product no longer in development. Long story short, it's messy.


There is a set of rules called Generally Accepted Accounting Procedures (GAAP) that address issues like this but I suspect there's a lot of latitude. I am not an accountant but do have some small business background. A long as I kept the IRS happy, I was happy.

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Offline OTV Booster

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Re: SpaceX Raptor LRE Proposed Successor: Project LEET-1337 LRE
« Reply #53 on: 09/27/2023 05:19 pm »
Giving it a different name was likely just part of the internal politics of the time; a way for Musk to clearly distinguish between the initiative he felt was failing, and the one he felt was the way forwards. Once he sorted out the underlying problem there was no need for 2 different engine design tracks, so no need for 2 different names.
I think he is being serious about a new engine.
Since the notional new engine is mentioned by Elon Musk as intended to help mankind become a multiplanetary species, I'm guessing that the Starship/Super Heavy would need to have the first stage modified to use as many as 12 engines with a total of 20 million pounds of thrust and the Starship portion fitted with five engines totaling 6 million pounds of thrust in order to burn enough fuel to reach portions of the solar system beyond Mars.
An F-1B thrust class next gen. engine would be perfect for a much larger next gen Starship system in the far future having the same engine counts for booster (33 engines) and ship (6 engines) as the current Starship system has.
Opinion:

I'd think they'd want to design a new engine to fit the current package, otherwise the thrust structures and plumbing would have to radically change. That's maybe 20-25% towards a new design. OTOH, maybe a new design is a development branch they're looking at.
We are on the cusp of revolutionary access to space. One hallmark of a revolution is that there is a disjuncture through which projections do not work. The thread must be picked up anew and the tapestry of history woven with a fresh pattern.

Offline steveleach

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Re: SpaceX Raptor LRE Proposed Successor: Project LEET-1337 LRE
« Reply #54 on: 09/27/2023 09:00 pm »
Giving it a different name was likely just part of the internal politics of the time; a way for Musk to clearly distinguish between the initiative he felt was failing, and the one he felt was the way forwards. Once he sorted out the underlying problem there was no need for 2 different engine design tracks, so no need for 2 different names.
I think he is being serious about a new engine.
Since the notional new engine is mentioned by Elon Musk as intended to help mankind become a multiplanetary species, I'm guessing that the Starship/Super Heavy would need to have the first stage modified to use as many as 12 engines with a total of 20 million pounds of thrust and the Starship portion fitted with five engines totaling 6 million pounds of thrust in order to burn enough fuel to reach portions of the solar system beyond Mars.
An F-1B thrust class next gen. engine would be perfect for a much larger next gen Starship system in the far future having the same engine counts for booster (33 engines) and ship (6 engines) as the current Starship system has.
Opinion:

I'd think they'd want to design a new engine to fit the current package, otherwise the thrust structures and plumbing would have to radically change. That's maybe 20-25% towards a new design. OTOH, maybe a new design is a development branch they're looking at.
I think people are reading way too much into something that happened a couple of years ago, and that everyone involved has probably moved on from now.

Offline DJPledger

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Re: SpaceX Raptor LRE Proposed Successor: Project LEET-1337 LRE
« Reply #55 on: 09/28/2023 08:43 pm »
Giving it a different name was likely just part of the internal politics of the time; a way for Musk to clearly distinguish between the initiative he felt was failing, and the one he felt was the way forwards. Once he sorted out the underlying problem there was no need for 2 different engine design tracks, so no need for 2 different names.
I think he is being serious about a new engine.
Since the notional new engine is mentioned by Elon Musk as intended to help mankind become a multiplanetary species, I'm guessing that the Starship/Super Heavy would need to have the first stage modified to use as many as 12 engines with a total of 20 million pounds of thrust and the Starship portion fitted with five engines totaling 6 million pounds of thrust in order to burn enough fuel to reach portions of the solar system beyond Mars.
An F-1B thrust class next gen. engine would be perfect for a much larger next gen Starship system in the far future having the same engine counts for booster (33 engines) and ship (6 engines) as the current Starship system has.
Opinion:

I'd think they'd want to design a new engine to fit the current package, otherwise the thrust structures and plumbing would have to radically change. That's maybe 20-25% towards a new design. OTOH, maybe a new design is a development branch they're looking at.
I think people are reading way too much into something that happened a couple of years ago, and that everyone involved has probably moved on from now.
So SpaceX will keep iterating Raptor and that LEET-1337 may have been cancelled or pushed back into the very far future. Perhaps SpaceX could go really radical and possibly dev. a RDRE after Raptor.

Offline OTV Booster

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Re: SpaceX Raptor LRE Proposed Successor: Project LEET-1337 LRE
« Reply #56 on: 10/09/2023 01:29 am »
Um, uh. What does RDRE mean?
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Offline chopsticks

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Re: SpaceX Raptor LRE Proposed Successor: Project LEET-1337 LRE
« Reply #57 on: 10/09/2023 01:41 am »
Probably rotating detonation something or other.

Offline KilroySmith

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Re: SpaceX Raptor LRE Proposed Successor: Project LEET-1337 LRE
« Reply #58 on: 10/09/2023 01:47 am »
I was going to be a snarky little whatever and point out the acronyms thread: https://forum.nasaspaceflight.com/index.php?topic=34802.0
But then I noticed that it doesn’t include that particular one.  And, unfortunately, I’m as in the dark as you are.

Offline Perchlorate

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Re: SpaceX Raptor LRE Proposed Successor: Project LEET-1337 LRE
« Reply #59 on: 10/09/2023 01:48 am »
Rotating Detonation Rocket Engine
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Tags: Raptor Starship 
 

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