Awww… nuts! Sad news about Reaction Engines. Another Great British space flight dream in the bin.

Back when I started this thread I was a massive Skylon fanboy after reading about it in Spaceflight magazine. Then I actually got around to reading my big Space Shuttle book by Dennis R. Jenkins and realized it wasn’t going to be as straight forward as chucking money at it!

Then SpaceX and Falcon 9 happened!!! :p
 

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That was exactly the same with me SteveO as to how I first saw anything about Skylon too through the BIS Spaceflight magazine and then onto the BIS Journal especially in the early years of its existence. I was somewhat of a fanboy as well I really wanted it to succeed where HOTOL failed but alas it was not to be. :(
 
Yep, SpaceX and Falcon 9 was that, oh yeah!, moment when I realized making routine space flight easy was about science and engineering and not looking cool!

Saying that, watching a Falcon 9 land is about as cool as it comes :cool:
 
Already for many years REL only spoke about using Skylon to "fly to Sydney in 4 hours" or "fly to New York in 2 hours", not for SSTO.

In 2008 they came up with LAPCAT-A2, which looks very much like Skylon, and in January 2011 they even announced that it could fly "within the next 15 years".
That should then be before the end of next year, but of course nothing happened since 2011. See attachments.
LAPCAT has been mentioned before in this topic in those years.

Falcon 9 did not kill REL, their total lack of any achievements did.
 

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  • LAPCAT-A2 Hypersonic airliner design by Reaction Engines (Air International March 2008).jpg
    LAPCAT-A2 Hypersonic airliner design by Reaction Engines (Air International March 2008).jpg
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  • LAPCAT-A2 could fly within 15 years (Air International January 2011).jpg
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  • SKYLON_Users_Manual_Rev_2.1.pdf
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There were two users manual released: one for the 275 tons Skylon C2, and another for the 325 tons D1. I have both of them on my HD, plus a ton of documents "Skylon for -" (space stations, Moon, Mars, upper stages, and other stuff).

SteveO has posted the later version of the Skylon user's manual, on configuration D1. Here (see attached PDF) is the earlier version that I have in my records, on configuration C2, if anybody is interested.
 

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  • Skylon.pdf
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And, as promised - here we go. Twenty files, max that can be attached to a post. More to come in the next message.

Note that the file called 6844338 is one of the Skylon user manual, sorry if it has already posted elsewhere with a different name.
It is the first manual, for the C-2 variant.
 

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  • IAC-10.B3.7.3 -.pdf
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  • IAC-10.D2.3.7.pdf
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  • IAC-10.D2.4.7.pdf
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  • IAC-11,B3,2,6,x10121 -.pdf
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  • IAC-11,B3,2,6,x10121.show.pdf
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  • IAC-11,D2,4,2,x10124.pdf
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  • IAC-13,D2,4,6,x19609.pdf
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  • IAC-14,A3,P,4,x23813 -.pdf
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  • IAC-14,D2,4,5,x25154 -.pdf
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  • IAC-09.D3.3.4.pdf
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  • IAC-09.D2.3.8 -.pdf
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  • 6.iac-04-iaa.3.6.2.08.pdf
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  • 110_Hempsell.pdf
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  • 6844338.pdf
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  • AFRL paper - Two Stage to Orbit Conceptual Vehicle Designs using the SABRE - Sept 2016.pdf
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  • Architecture and Ground operations concept for a Two Stage To Orbit using SABRE enginesand lau...pdf
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  • bond.pdf
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  • Design of an orbital base facility for complex missions IAC 08 D3.3.1.pdf
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  • Dr-Robert-Bond-presentation.pdf
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  • IAC-05-D3.3.06.pdf
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Second part. Twelve more files. SKYLON_Users_Manual_Rev_2.1 is the other one: the D-1 variant.
 

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  • IAC-14,E6,3,8,x25083 -.pdf
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  • JBIS_v60_188-196.pdf
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  • JBIS_v56_118-126.pdf
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  • JBIS_v56_108-117.pdf
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  • IAC-15,D2,1,8,x31601.pdf
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  • LAPCAT.pdf
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  • Mark-Hempsell-Publications-List.pdf
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  • scribd.vpdfs.com_skylon-technical-report-skylon-assessment-report-pub.pdf
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  • mars_troy.pdf
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  • SKYLON_Users_Manual_Rev_2.1.pdf
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  • skylon-assessment-report-pub.pdf
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  • The Synergetic Air-Breathing Rocket Engine SABRE - Development Status Update-IAC-20,C4,7,1,x60...pdf
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It’s interesting to compare the rocket plumes on the original Skylon mission animation and Hazegrayart’s more recent go at it! :D
They look cool, but aren't simulations of what the plume actually does. At altitude with lower pressure then it looks more like the attached. Which may cause issues for the aft fuselage structure and thin, brittle TPS covering it...
 

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Scott Manley said:
How Britain's Air Breathing Rocket Engine Would Have Worked... If The Builder Hadn't Gone Bankrupt.
Reaction Engines had been working on an innovative engine design named SABRE, this was intended to operate as an air breathing engine up to about mach 5 and then switch to a pure rocket engine cycle. The ultimate goal was to build an aircraft named 'Skyline' which could fly all the way to orbit without dropping stages, but the company was first and foremost focussed on demonstrating the engine design, and in particular, the pre-cooler which would be required to chill the incoming air down to usable temperatures so it could be compressed and then used to burn hydrogen in a rocket engine. [...]
Video:
View: https://youtu.be/4YLg8X0BAL0?si=d80Tq6TIxXR3p3Ch

Link:
Code:
https://youtu.be/4YLg8X0BAL0?si=d80Tq6TIxXR3p3Ch
 
My post # 617 in this thread three weeks ago got several likes (thank you), but nobody here has been able to answer the question therein about whether or not the planned British test program (to add a Reaction Engines' helium precooler in front of an EJ200 jet engine as used in the Eurofighter Typhoon) actually occurred in 2019-21. I am now doubtful that it ever did, even though the test appears to have already been fully funded. I re-read my sources. Craig Hoyle wrote the article "EJ200 trial to accelerate UK hypersonics research" in the 31 July 2019 issue of Flight International. Aviation Week's London correspondent Tony Osborne wrote "Precooler Technology Could Bring Advantages to Fighter Engines" (AWST 19 August 2019), which followed up from his colleague Guy Norris's "Positive Reaction (Reaction Engines' Pre-Cooler Passes Mach 3.3 Test [in Colorado])" (AWST 22 April 2019). I have emailed queries about the planned test program directly to Mr Hoyle and Mr Osborne, and await their response—or better yet, an answer included in an upcoming informative article by one or both of them about the life and death of Reaction Engines.

I completely agree (in fact ever since the 1990's when I learned of Skylon) with what the famed Henry Spencer wrote on a newsgroup recently, that it would have been wiser for Reaction Ltd to use its constrained funds to build "a crude-and-heavy test aircraft to put the engine through its paces, running out of fuel and oxidizer just after the shift to rocket mode... [Reaction] needed to get something flying without spending several billion dollars first... nobody was ever going to give them billions on the strength of paper studies. They spent far too long trying to sell that impossible fantasy."

Still, the end of Reaction Engines is a loss for space achievement. Maybe whomever inherits the defunct company's intellectual property will make something of it.
 
Let's wait and see Owens Z, It would be such a waste to see all the technology just disappear and not be used for something else.
 

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