Author Topic: The Reaction Engines Skylon/SABRE Master Thread (6)  (Read 448501 times)

Offline Asteroza

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Re: The Reaction Engines Skylon/SABRE Master Thread (6)
« Reply #580 on: 06/02/2017 01:57 am »
Another application is for some proposed intercooler/recuperation circuits for advanced turbofans, such as the Ultrafan research in europe, particularly MTU and friends incolved in CLAIRE, CRISP,and GTF work.

http://www.newac.eu

Many of these proposal have a recuperator heat exchanger in the turbine exhaust flowpath. But that's pretty hot gas on both sides. The microchannel work of the SABRE precooler has some dependency on the immense heatsink of cryogenic fluid, to keep such small tubes from otherwise melting.

Offline JCRM

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Re: The Reaction Engines Skylon/SABRE Master Thread (6)
« Reply #581 on: 06/02/2017 06:57 pm »
This month's BIS Spaceflight magazine has a 2 page + pictures piece on SABRE entitled "Hypersonic Strike or Reusable Launch Vehicle?"
The author is uncredited, and no sources are given, however I am under the impression there is a close relationship between REL and the BIS, so it may reveal some interesting insights.

After some background (ASP and LACES, HOTOL and RB545) the article mentions
Quote from: Spaceflight vol 59 No 7, July 2017 (ISSN 0038-6340), p 244
... under the name SABRE the new engine [...] bring[s] many applications from a single and highly defined design originally developed for one purpose [Skylon] - that apparent bonus [...] presents problems as to where to position the SABRE as it slashes through conventional ways of carrying out a multitude of roles.

The article goes on to mention the 2014-2016 ARFL analysis of the engine, leading on to claiming that after the USAF indicated no current requirement for SSTO 
Quote from: p 245
... no plans to implement a programme of that scale in the immediate future. Supporting the ARFL, Reaction Engines defined plans for a demonstrator based on the broader conclusions drawn up by the Air Force, [as] one component of a two stage satellite launcher
leading to the two TSTO concepts from SpaceWorks Enterprosed in conjunction with the ARFL's High-Speed Systems Division. I emphasised the section which suggests more REL involvement in developing the TSTO concepts than I was previously aware.

The piece gives the thrust of the demonstrator engine as 44000 lbf, down from the 150000 lbf planned for a Skylon engine. The article suggests
Quote from: p 246
This should speed the process of building and testing and display a better fit with some unexpected applications which the US Air Force is currently examining. [the TSTOs] as well as a hypersonic X-series research craft or even, via an intermediate step, to a combat air vehicle capable of speeds in excess of Mach 4.5
which hints at it being a far more targeted reduced scale demonstrator than simply making it about a quarter of the size.

The article then suggests
Quote
The reduced scale engine will also effect a better fit between the Jet engine and the rocket engine and through a three-step test process could find real applications in the US or Europe in the late 2020s

A time line for the testing is laid out, the first step being the core and heat exchangers being tested to 2020, then an integrated engine in 2020-2021 as the second step, and the third step of test flights following that. This is a tighter timeframe for the second step than I had picked up on previously.

The article concludes
Quote
it is quite possible that the SABRE engine will find its first application as a propulsion system for a Mach 4+ hemispheric strike or intercept system, a role being developed by the US Air Force [...] Only then might it be adopted for a satellite launcher


I feel the article is broadly in line with my understanding that something like Skylon is still the goal of those behind SABRE, but a much more pragmatic path is being taken to get there than the one envisioned by the engineers with their focus on the lowest overall development cost.

Offline Star One

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Re: The Reaction Engines Skylon/SABRE Master Thread (6)
« Reply #582 on: 06/02/2017 07:27 pm »
There's also some interesting illustrations with the article.

Offline t43562

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Re: The Reaction Engines Skylon/SABRE Master Thread (6)
« Reply #583 on: 06/04/2017 06:45 am »
This month's BIS Spaceflight magazine has a 2 page + pictures piece on SABRE entitled "Hypersonic Strike or Reusable Launch Vehicle?"
I can't see it in the contents on the website so I was wondering if you mean Spaceflight Vol 59 No 06 or No 05 ? I just want to be absolutely sure before I purchase it.

The shop is here for anyone else who might want to buy it:
http://www.bis-space.com/eshop/products-page/publications/spaceflight/spaceflight-2017/
« Last Edit: 06/04/2017 06:46 am by t43562 »

Offline paddybloomfield

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Re: The Reaction Engines Skylon/SABRE Master Thread (6)
« Reply #584 on: 06/04/2017 09:10 am »
It's Vol 59 No 7 July 2017

Offline SICA Design

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Re: The Reaction Engines Skylon/SABRE Master Thread (6)
« Reply #585 on: 06/04/2017 09:10 am »
It's Vol 59 No 7 July 2017 on the front cover - good article!

Offline john smith 19

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Re: The Reaction Engines Skylon/SABRE Master Thread (6)
« Reply #586 on: 06/04/2017 12:01 pm »
So the program is delayed again by another year, I thought the full engine was meant to be going under testing in 2019?
It's interesting to note that when REL has been fully funded they have delivered what they said they could deliver when they said they could deliver it.

This may come as a bit of a shock to commercial investors, who are more used to being promised the Earth, Moon and stars. REL don't. Perhaps they should since it seems to be what is expected.

REL's concept remains the only design that has the potential to put "on demand" reusable launch into the hands of anyone capable of operating their system. That's probably the only way to achieve the massive cost reductions that will make space access truly affordable, and thereby get those concepts for materials mfg in space out of peoples bottom desk drawers (or their cloud archives) and actually into orbit.  :(
MCT ITS BFR SS. The worlds first Methane fueled FFSC engined CFRP SS structure A380 sized aerospaceplane tail sitter capable of Earth & Mars atmospheric flight.First flight to Mars by end of 2022 2027?. T&C apply. Trust nothing. Run your own #s "Extraordinary claims require extraordinary proof" R. Simberg."Competitve" means cheaper ¬cheap SCramjet proposed 1956. First +ve thrust 2004. US R&D spend to date > $10Bn. #deployed designs. Zero.

Offline t43562

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Re: The Reaction Engines Skylon/SABRE Master Thread (6)
« Reply #587 on: 06/06/2017 12:08 pm »
From the REL job adverts I think it's fairly obvious that the spin off product is heat exchanger related:

https://www.reactionengines.co.uk/vacancy/future-projects-thermal-engineer/
https://www.reactionengines.co.uk/vacancy/future-projects-development-engineer/

It would seem that spin-offs are to be taken care of by "Future Projects" and I think some of the skills are indicative:

Quote
Experience with any of:
    High pressure fluids and control systems
    Electrical control systems and instrumentation
    Rotating machinery, High temperature combustion systems
    Advanced manufacturing processes i.e. Vacuum brazing, additive manufacture

Exposure to space or aerospace systems engineering

...and...

Quote
Knowledge and experience of a broad variety of heat exchangers
Experience in the implementation of mechanical design of heat exchangers

Offline Zingpc

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Re: The Reaction Engines Skylon/SABRE Master Thread (6)
« Reply #588 on: 06/11/2017 09:41 am »
Hi, my first time on these excellent forums. Considering L2, but am tired of space history, a long while ago when we were all hopeful. We have seen fourty years of corporate extraction of the most dollars from the ultimate sucker. 

My dreams for Skylon: that someone with dozens of billions to risk, hooks up with others of the billionaire club ( thousands of them) and funds Skylon and say a two stage 100 tonne payload variant. It would be so cool to have British genius and engineering create the serious lift (I refuse to call greater than a sea container load super heavy) that goes beyond tin can space flight.

However reality is likely this will just play out as spinoff products.
« Last Edit: 06/11/2017 09:45 am by Zingpc »

Offline t43562

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Re: The Reaction Engines Skylon/SABRE Master Thread (6)
« Reply #589 on: 06/13/2017 07:53 pm »

This is a link to today's lecture - hope it isn't just livestream but post-live as well! :-)

Barnwell  Lecture, 13 June 2017

You need to skip the first 15 minutes of faffing.

https://uwe.cloud.panopto.eu/Panopto/Pages/Viewer.aspx?id=0866a3cb-5efb-4ca1-a2a7-23fc41f82b8b

Offline Dao Angkan

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Re: The Reaction Engines Skylon/SABRE Master Thread (6)
« Reply #590 on: 06/13/2017 10:03 pm »
Excellent, and in my back yard, a shame that I had to work. Clearly a recruitment drive, for those that don't know, UWE (University of Western England) is located right next to Bristol's (technically Filton's) aerospace industry. Rolls Royce, BAE, and Airbus are all located there, employing many thousands. Reaction Engines are currently recruiting ~1-2 people a week, so not a huge recruitment drive, but for a company of 120 it's significant.

He comments on significant stuff from around 55 minutes such as spin off technologies, outside investment, and how BAE offer more than just financial help.

And yes, it was a very sunny tuesday evening here :p
« Last Edit: 06/13/2017 10:17 pm by Dao Angkan »

Offline Dao Angkan

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Re: The Reaction Engines Skylon/SABRE Master Thread (6)
« Reply #591 on: 06/13/2017 10:41 pm »
Milestones (slightly paraphrased for brevity);

Quote
So the pre-cooler does this job; simplistically, it takes 1000° air and cools it to -150° in a fraction of a second. To prove that fully we have to take that to a hot wind tunnel which we don't have here regularly here in the UK. That is a big milestone that is coming up for the company in the next 8-10 months.
« Last Edit: 06/13/2017 10:43 pm by Dao Angkan »

Offline Dao Angkan

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Re: The Reaction Engines Skylon/SABRE Master Thread (6)
« Reply #592 on: 06/13/2017 10:57 pm »
Manufacturing;

Quote
We have had to invest a lot in manufacturing capability. This is a really impressive piece of kit, a vacuum furnace that we've designed ourselves ... an ultra-clean, ultra- high vacuum facility for joining heat exchangers. So these heat exchangers contain many kms, hundreds, if not thousands kms of tubing that's a mm in diameter, with real thicknesses of less than 30 microns containing high pressure helium, 200 bar pressure helium, and they have to be joined in a completely leak-tight way, and to survive in this very aggressive environment, and it's a difficult alloy to handle, so we needed to make this investment.
« Last Edit: 06/13/2017 10:58 pm by Dao Angkan »

Offline Dao Angkan

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Re: The Reaction Engines Skylon/SABRE Master Thread (6)
« Reply #593 on: 06/13/2017 11:22 pm »
Spin off technologies;

Quote
So we do a lot of technology development in the program; heat exchangers being a key element. One of the attractions of me joining the company ... I had no intention of leaving Rolls Royce, but Sabre was too good an opportunity to miss in a hi-tech growing company, but the technology, I knew, had wider applications. I can't really tell you what we're pursuing at the moment, specifically, but in terms of heat exchangers, we are working in these territories (graphic). We are not going after the heat exchangers business', it's far too aggresive, it's far too commercial. But we have heat exchangers that are high performance - they're very compact, they're extremely light-weight, because of the space requirements, where 1g saved of a heat exchanger converts to kgs of payload at the top end.

So we're looking at things like onboard power generation, the ability to use heat energy in different ways, satellite thermal control, improving aero-engines (mentions Rolls Royce people in the audience), definitely an opportunity to get heat exchangers into aero-engines. Not previously used due to being big and heavy ... also motorsport, hybrid electric vehicles, and novel cycles for power generation ... a very very interesting area.
« Last Edit: 06/13/2017 11:29 pm by Dao Angkan »

Offline Dao Angkan

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Re: The Reaction Engines Skylon/SABRE Master Thread (6)
« Reply #594 on: 06/13/2017 11:52 pm »
Investment:

Who's going to fly your engine?

Quote
A lot of people asking about how much SpaceX is a competitor, they see as a potential customer...

In his presentation about "new space" he shows how first stage recovery will reduce the cost of space access ... impression is that SABRE will help to reduce by a further order of magnitude (or maybe "just" x5 if booster recovery is routine)

Quote
They need more investment, won't say how much, but maybe some billions (joke?). Going to be a company of two parts ... SABRE ... the engine company ... and a seperate spin off technology company. Spin off company needs to make money, SABRE can be more blue skies .... 18/20 can fail. Spin off company needs to be more succesful.

Quote
Cost to LEO  a moving target .... original aim to be an order of magnitude cheaper ($10k/kg) ... but now re-use might bring that down to $5k/kg ... they're aiming for $1k/kg. He thinks that first stage re-use might reduce cost by half .... I think that's a fair estimate.
« Last Edit: 06/14/2017 12:14 am by Dao Angkan »

Offline ChrisWilson68

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Re: The Reaction Engines Skylon/SABRE Master Thread (6)
« Reply #595 on: 06/14/2017 01:26 am »
So the program is delayed again by another year, I thought the full engine was meant to be going under testing in 2019?
It's interesting to note that when REL has been fully funded they have delivered what they said they could deliver when they said they could deliver it.

This may come as a bit of a shock to commercial investors, who are more used to being promised the Earth, Moon and stars. REL don't. Perhaps they should since it seems to be what is expected.

REL's concept remains the only design that has the potential to put "on demand" reusable launch into the hands of anyone capable of operating their system. That's probably the only way to achieve the massive cost reductions that will make space access truly affordable, and thereby get those concepts for materials mfg in space out of peoples bottom desk drawers (or their cloud archives) and actually into orbit.  :(

The only concept?  If you want to root for Skylon, fine, but don't disparage the alternatives by claiming Skylon is the only one.

SpaceX's ITS and Blue Origin's New Glenn both plan to be all these things.  Both fully-reusable.  Both at least as cheap and easy to operate as Skylon.  Both can launch on demand with fast turn-around time.  Both plan to change the world with a radical reduction in launch costs.

Skylon is not the only game in town.

Offline ChrisWilson68

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Re: The Reaction Engines Skylon/SABRE Master Thread (6)
« Reply #596 on: 06/14/2017 01:42 am »
Quote
Cost to LEO  a moving target .... original aim to be an order of magnitude cheaper ($10k/kg) ... but now re-use might bring that down to $5k/kg ... they're aiming for $1k/kg. He thinks that first stage re-use might reduce cost by half .... I think that's a fair estimate.

Falcon 9 today is advertised as $62 million for 5.5 tons to GTO.  They claim a fully-expendable GTO capability of 8.3 tons.  So two thirds of the payload if not expendable.  Applying that to the expendable 22.8 tons to LEO gives 15 tons to LEO for $62 million, or $4.1k/kg.  Falcon Heavy is quoted as about 3 times the payload for 1.5x the cost, so it's roughly $2k/kg.

So if they're aiming for $1k/kg to LEO, they're only aiming for 2x better than Falcon Heavy pricing today.  That doesn't leave them much room for error or for SpaceX getting better.  And that doesn't even consider ITS or Blue Origin's New Glenn, both of which are meant to be fully reusable and far cheaper than Falcon 9 and Falcon Heavy per kg.

Offline t43562

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Re: The Reaction Engines Skylon/SABRE Master Thread (6)
« Reply #597 on: 06/14/2017 08:33 am »
So the program is delayed again by another year, I thought the full engine was meant to be going under testing in 2019?
It's interesting to note that when REL has been fully funded they have delivered what they said they could deliver when they said they could deliver it.

This may come as a bit of a shock to commercial investors, who are more used to being promised the Earth, Moon and stars. REL don't. Perhaps they should since it seems to be what is expected.

REL's concept remains the only design that has the potential to put "on demand" reusable launch into the hands of anyone capable of operating their system. That's probably the only way to achieve the massive cost reductions that will make space access truly affordable, and thereby get those concepts for materials mfg in space out of peoples bottom desk drawers (or their cloud archives) and actually into orbit.  :(

The only concept?  If you want to root for Skylon, fine, but don't disparage the alternatives by claiming Skylon is the only one.

SpaceX's ITS and Blue Origin's New Glenn both plan to be all these things.  Both fully-reusable.  Both at least as cheap and easy to operate as Skylon.  Both can launch on demand with fast turn-around time.  Both plan to change the world with a radical reduction in launch costs.

Skylon is not the only game in town.

Weren't the words "on demand" pretty important there? Isn't the idea that you can launch and turn around quickly part of the idea? It would be interesting to ask if anyone on the SpaceX and New Glen discussions is busy reminding people there that "they're not the only games in town". 

Offline SICA Design

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Re: The Reaction Engines Skylon/SABRE Master Thread (6)
« Reply #598 on: 06/14/2017 10:25 am »
So the program is delayed again by another year, I thought the full engine was meant to be going under testing in 2019?
It's interesting to note that when REL has been fully funded they have delivered what they said they could deliver when they said they could deliver it.

This may come as a bit of a shock to commercial investors, who are more used to being promised the Earth, Moon and stars. REL don't. Perhaps they should since it seems to be what is expected.

REL's concept remains the only design that has the potential to put "on demand" reusable launch into the hands of anyone capable of operating their system. That's probably the only way to achieve the massive cost reductions that will make space access truly affordable, and thereby get those concepts for materials mfg in space out of peoples bottom desk drawers (or their cloud archives) and actually into orbit.  :(

The only concept?  If you want to root for Skylon, fine, but don't disparage the alternatives by claiming Skylon is the only one.

SpaceX's ITS and Blue Origin's New Glenn both plan to be all these things.  Both fully-reusable.  Both at least as cheap and easy to operate as Skylon.  Both can launch on demand with fast turn-around time.  Both plan to change the world with a radical reduction in launch costs.

Skylon is not the only game in town.

Weren't the words "on demand" pretty important there? Isn't the idea that you can launch and turn around quickly part of the idea? It would be interesting to ask if anyone on the SpaceX and New Glen discussions is busy reminding people there that "they're not the only games in town".

"...into the hands of anyone capable of operating their system" is also a key difference with their operating model: an owner/operator launching their own payloads pays the cost, not the price.

Offline oldAtlas_Eguy

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Re: The Reaction Engines Skylon/SABRE Master Thread (6)
« Reply #599 on: 06/14/2017 03:34 pm »
If you finally get to the SSTO HTHL situation then Skylon being a product supplier like Boeing selling the craft and letting others (several others that compete against each other) operate it makes sense. But until then being an all of the above developer/manufacturer/owner/operator will be the opening round. The vehicle must prove its capabilities and even more so its business case.

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