Author Topic: Vulcan SMART Reuse  (Read 98638 times)

Offline FutureSpaceTourist

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Re: Vulcan SMART Reuse
« Reply #240 on: 11/10/2023 05:51 pm »
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Remember the LOFTID half scale engine reuse demo last year?

https://twitter.com/torybruno/status/1723027144245182613

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Here's some sea trials (not orbital) at full scale.  #VulcanRocket

Offline TrevorMonty

Re: Vulcan SMART Reuse
« Reply #241 on: 11/11/2023 09:32 am »
Helicopter drop tests next ?

Offline FutureSpaceTourist

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Re: Vulcan SMART Reuse
« Reply #242 on: 11/11/2023 11:52 am »
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Hi Tory! What exactly are we looking at here? 👍😮👍

https://twitter.com/torybruno/status/1723318306352832822

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Full scale (representative of 2 BE4 engines inside the thrust structure) in a sea keeping and recovery test

https://twitter.com/torybruno/status/1723027142106063105

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Remember the LOFTID half scale engine reuse demo last year?

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I was wondering if there were any more tests on that. Is it scheduled for any Vulcan launches?

https://twitter.com/torybruno/status/1723320072872079770

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Soo many tests. This was not the first.  My ITAR and IP lawyers are being very careful (ie: doing their job).  I’ll do my best to keep these tidbits bits coming

Edit to add:

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Did it live up to your expectations and what stage is the program at now?

https://twitter.com/torybruno/status/1723327500623679692

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exceeded
« Last Edit: 11/11/2023 12:12 pm by FutureSpaceTourist »

Offline FutureSpaceTourist

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Re: Vulcan SMART Reuse
« Reply #243 on: 11/11/2023 12:11 pm »
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Can you see a future where you are fully resuable? Or does it not make financial sense to do so?

Awesome to see this trial.

https://twitter.com/torybruno/status/1723326481915330891

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If I add a LEO optimized rocket to the stable.

Online greybeardengineer

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Re: Vulcan SMART Reuse
« Reply #244 on: 11/11/2023 01:16 pm »
Funny how an architecture chosen and optimized primarily around colonizing Mars has according to Tory "little to zero" launch capability above LEO. At least he finally stopped proclaiming first stage reuse was uneconomical.  ::)

Offline TrevorMonty

Re: Vulcan SMART Reuse
« Reply #245 on: 11/11/2023 05:06 pm »


https://twitter.com/free_space/status/1549094136342630400

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Coming up next issue @AviationWeek: @ulalaunch modifies plan for Vulcan rocket BE-4 recovery--drops helicopter, will let engines, surrounded by inflatable aeroshell decelerator, splash down in ocean. "It turns out the decelerator makes an excellent raft,” says @torybruno.

Wow


First Blue takes a page from SpaceX’s stationary ASDSs.
Now ULA may be learning from SpaceX’s floating fairing halves.

:)

However, this is heading OT for ”as announced/built”.
ULA is still a long way from even testing this.

Would be nice if Rocket lab could drop the helicopter catch on Electron too.

Found this post by chance. Then had to scroll through 100 odd posts in jul22 to find it again.

jstrotha0975, RL have taken your advice onboard.

Offline deltaV

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Re: Vulcan SMART Reuse
« Reply #246 on: 11/11/2023 05:32 pm »
https://twitter.com/torybruno/status/1723326481915330891

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If I add a LEO optimized rocket to the stable.

I wonder if Tory wants to add a "LEO optimized" fully reusable rocket to ULA's stable but is held back by ULA's owners not wanting to fund it.

Funny how an architecture chosen and optimized primarily around colonizing Mars has according to Tory "little to zero" launch capability above LEO. At least he finally stopped proclaiming first stage reuse was uneconomical.  ::)

I think a better version of Tory's argument is that two stage vehicles such as Starship, New Glenn, and Terran R can only do GEO with an added third stage, propellant transfer, or in-orbit assembly. A third stage would likely only be used for a few military missions so it wouldn't get enough usage to get great reliability. Propellant transfer and in-orbit assembly have yet to be proven and may not be reliable. So all options have downsides, though I don't think those downsides are important enough for Vulcan to make sense overall.

Offline FutureSpaceTourist

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Re: Vulcan SMART Reuse
« Reply #247 on: 04/06/2024 03:09 pm »
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Hey @torybruno 👋,wanted to ask a question.Will Vulcan in it's second flight include reusability of engines or that would be performed after 3 to 4 flights??

https://twitter.com/torybruno/status/1776627972457312640

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No. Too soon. The timing of the first experimental engine recoveries and implementation is in work with the customers that are impacted by it

Offline Robert_the_Doll

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Re: Vulcan SMART Reuse
« Reply #248 on: 06/15/2024 04:00 am »
https://twitter.com/MTrider16/status/1801694671602913369
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Looks really good.  Is there a flight picked out yet for SMART?

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Yes

« Last Edit: 06/15/2024 05:10 am by FutureSpaceTourist »

Offline FutureSpaceTourist

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Re: Vulcan SMART Reuse
« Reply #249 on: 06/15/2024 05:09 am »
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Wen SMART reuse?

https://twitter.com/torybruno/status/1801805170923421774

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After a few flights to measure environments and some demos to confirm key design elements.  We recently held a very successful PDR and are moving on towards CDR.

Offline FutureSpaceTourist

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Re: Vulcan SMART Reuse
« Reply #250 on: 07/05/2024 03:47 pm »
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@torybruno
what is the max amount of times a SMART engine pod can be reused?

https://twitter.com/torybruno/status/1809252314277912792

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3 is economically attractive. I’d like to get as many as 10. Well know when we start gathering data

Offline FutureSpaceTourist

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Re: Vulcan SMART Reuse
« Reply #251 on: 08/10/2024 10:21 pm »
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Hey Tory! When can we expect to see SMART reuse in action?

https://twitter.com/torybruno/status/1822397294882566625

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Working towards a CDR this year. That will be followed by a couple of flight experiments/demos. The implementation target date will get firmed up in that time frame
« Last Edit: 08/10/2024 10:21 pm by FutureSpaceTourist »

Offline ZachF

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Re: Vulcan SMART Reuse
« Reply #252 on: 08/16/2024 01:09 pm »
Funny thought I had... I wonder if the cost of a Raptor 3 is now less than the SMART recovery cost of BE-4?
artist, so take opinions expressed above with a well-rendered grain of salt...
https://www.instagram.com/artzf/

Offline Starshipdown

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Re: Vulcan SMART Reuse
« Reply #253 on: 08/16/2024 07:32 pm »
Funny thought I had... I wonder if the cost of a Raptor 3 is now less than the SMART recovery cost of BE-4?

Apples to oranges comparison.

The problem with that line of thinking is that it leaves out the critical context that Raptor 3 is being produced solely in-house for SpaceX itself, not for another company as is the case with BE-4 for ULA.

A more direct comparison would be Raptor to BE-4 marginal cost comparison. Even if ULA was buying Raptors, SpaceX likely would have to charge them significantly more than what SpaceX makes them for.

Offline seb21051

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Re: Vulcan SMART Reuse
« Reply #254 on: 08/17/2024 09:37 pm »
Funny thought I had... I wonder if the cost of a Raptor 3 is now less than the SMART recovery cost of BE-4?

Apples to oranges comparison.

The problem with that line of thinking is that it leaves out the critical context that Raptor 3 is being produced solely in-house for SpaceX itself, not for another company as is the case with BE-4 for ULA.

A more direct comparison would be Raptor to BE-4 marginal cost comparison. Even if ULA was buying Raptors, SpaceX likely would have to charge them significantly more than what SpaceX makes them for.

Just imagine what SX could charge for comparative specs such as these, with BO purported to be asking ULA $7 million per BE-4 copy. Marginal cost would be an interesting comparison.

                              Raptor 3                          BE-4
Mass                      1525kg                  est 3,500kg
Thrust                       280 tf                  250 tf  (MKS tons)
Chamber Pressure     350 bar                134 bar
Vac Specific Impulse  350s                    339s
Thrust to Weight      187                        78
Thrust Density           215.4tf/m2            92.6tf/m2 of nozzle
mdot at equal p        800                       737  kg/sec
nozzle exit area        1.3                                  2.6  m2
« Last Edit: 08/17/2024 09:55 pm by seb21051 »

Offline dglow

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Re: Vulcan SMART Reuse
« Reply #255 on: 08/18/2024 04:05 pm »
Funny thought I had... I wonder if the cost of a Raptor 3 is now less than the SMART recovery cost of BE-4?

Apples to oranges comparison.

The problem with that line of thinking is that it leaves out the critical context that Raptor 3 is being produced solely in-house for SpaceX itself, not for another company as is the case with BE-4 for ULA.

A more direct comparison would be Raptor to BE-4 marginal cost comparison. Even if ULA was buying Raptors, SpaceX likely would have to charge them significantly more than what SpaceX makes them for.

@ZachF's original observation was Apples to Oranges too. That the recovery cost of one, already-manufactured engine could be greater than the cost for a competitor to build an entirely new engine from scratch... think about that.

The in-house nature of Raptor's cost is worth noting... but the cost of SMART recovery would also be in-house.

Offline AmigaClone

Re: Vulcan SMART Reuse
« Reply #256 on: 08/18/2024 06:34 pm »
Funny thought I had... I wonder if the cost of a Raptor 3 is now less than the SMART recovery cost of BE-4?

Apples to oranges comparison.

The problem with that line of thinking is that it leaves out the critical context that Raptor 3 is being produced solely in-house for SpaceX itself, not for another company as is the case with BE-4 for ULA.

A more direct comparison would be Raptor to BE-4 marginal cost comparison. Even if ULA was buying Raptors, SpaceX likely would have to charge them significantly more than what SpaceX makes them for.

@ZachF's original observation was Apples to Oranges too. That the recovery cost of one, already-manufactured engine could be greater than the cost for a competitor to build an entirely new engine from scratch... think about that.

The in-house nature of Raptor's cost is worth noting... but the cost of SMART recovery would also be in-house.

The cost of SMART recovery might not be entirely in-house, but would depend on if ULA owned the assets used in the recovery or if they were contracted out. Also, going beyond the recovery, would any refurbishment the engines recovered by SMART be done in-house?

Offline punder

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Re: Vulcan SMART Reuse
« Reply #257 on: 08/18/2024 07:07 pm »
Where the costs come from in the supply chain is irrelevant to the customer who must decide which launch provider to use in terms of price, schedule and match to customer needs… am I missing something? Seriously.

Offline AmigaClone

Re: Vulcan SMART Reuse
« Reply #258 on: 08/19/2024 06:00 am »
Where the costs come from in the supply chain is irrelevant to the customer who must decide which launch provider to use in terms of price, schedule and match to customer needs… am I missing something? Seriously.

True, but after the contract between the launch provider and the customer is signed, it's in the launch provider's interest to prevent those costs from increasing excessively even if that contract is not a fixed price one. That might be easier with a supply chain that is more in-house than one that depends on outside suppliers for significant parts of their launch vehicle.

Offline LouScheffer

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Re: Vulcan SMART Reuse
« Reply #259 on: 08/19/2024 11:15 pm »
From the Media Teleconference today:
Crew 9's booster will fly first on a Starlink mission to ensure that the moisture intrusion into its fuel and LOX tank had no effect. The tanks had to be dried out and some components replaced.
NASA are clearly pleased that they’re able to take advantage of a Starlink flight to prove out the Crew-9 booster. A rare known case of positively wanting a flight proven booster. (Given that another brand new booster presumably wouldn’t be available in time.)
In one of the few cases where a customer has explicitly requested re-usability, SMART does not help.  There are no fight-proven tanks in SMART, since they are new for every mission.

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