Also I might be reading this wrong but there is some implication that their engine has a Thrust-to-Weight ratio of around 450
Really it depends on what the definition of engine mass includes. I'd believe the TWR of 450 for just the combustion chamber, maybe even including the instrumentation & sensors. But if you consider TVCs part of it, or control avionics, or turbopumps (which surely ought to be) then it would drop to something more sane.
My instinct is a) The engine is pressure fed, which raises the tank mass substantially (unless it's a flometrix style reciprocating pump driven by a smallish high pressure third tank) b) It's a typo. Occams razor says it's b) pending confirmation that the company is serious about that T/W ratio.
Here's what the page said:"Weighing just 7.5 kilos, this engine can lift 3.5 tonnes."That's a thrust to weight ratio of 467. Not sure where the typo could be.
Quote from: john smith 19 on 11/20/2019 09:10 pmMy instinct is a) The engine is pressure fed, which raises the tank mass substantially (unless it's a flometrix style reciprocating pump driven by a smallish high pressure third tank) b) It's a typo. Occams razor says it's b) pending confirmation that the company is serious about that T/W ratio. From this recruitment notice of theirs from last year (only the google cache available sorry) it looks like we can rule out option (a)!https://webcache.googleusercontent.com/search?q=cache:k4NSoCLQvyMJ:https://orbex.space/assets/uploads/documents/Orbex-TPA2018-Job-Specification.pdf
Launch integrator TriSept Corp. announced plans Jan. 14 to purchase an Orbex Prime launch vehicle for a dedicated rideshare mission to fly from Scotland’s Sutherland Spaceport in 2022.
Quote from: gmbnz on 11/20/2019 10:06 pmQuote from: john smith 19 on 11/20/2019 09:10 pmMy instinct is a) The engine is pressure fed, which raises the tank mass substantially (unless it's a flometrix style reciprocating pump driven by a smallish high pressure third tank) b) It's a typo. Occams razor says it's b) pending confirmation that the company is serious about that T/W ratio. From this recruitment notice of theirs from last year (only the google cache available sorry) it looks like we can rule out option (a)!https://webcache.googleusercontent.com/search?q=cache:k4NSoCLQvyMJ:https://orbex.space/assets/uploads/documents/Orbex-TPA2018-Job-Specification.pdfPressure feds have some attractions for upper stages. OTOH 3.5tonnes is well over the line where turbo machinery is a good choice (rather than reciprocating pumps)
Quote from: john smith 19 on 11/21/2019 07:28 amQuote from: gmbnz on 11/20/2019 10:06 pmQuote from: john smith 19 on 11/20/2019 09:10 pmMy instinct is a) The engine is pressure fed, which raises the tank mass substantially (unless it's a flometrix style reciprocating pump driven by a smallish high pressure third tank) b) It's a typo. Occams razor says it's b) pending confirmation that the company is serious about that T/W ratio. From this recruitment notice of theirs from last year (only the google cache available sorry) it looks like we can rule out option (a)!https://webcache.googleusercontent.com/search?q=cache:k4NSoCLQvyMJ:https://orbex.space/assets/uploads/documents/Orbex-TPA2018-Job-Specification.pdfPressure feds have some attractions for upper stages. OTOH 3.5tonnes is well over the line where turbo machinery is a good choice (rather than reciprocating pumps)It is and you're right. Orbex has been recruiting Turbomachinery engineers for years, and I have it on good authority that they've recently "finished" their assembly- at least to the point where they're ready to begin testing.
Quote from: TartanPump on 03/17/2020 03:12 pmQuote from: john smith 19 on 11/21/2019 07:28 amQuote from: gmbnz on 11/20/2019 10:06 pmQuote from: john smith 19 on 11/20/2019 09:10 pmMy instinct is a) The engine is pressure fed, which raises the tank mass substantially (unless it's a flometrix style reciprocating pump driven by a smallish high pressure third tank) b) It's a typo. Occams razor says it's b) pending confirmation that the company is serious about that T/W ratio. From this recruitment notice of theirs from last year (only the google cache available sorry) it looks like we can rule out option (a)!https://webcache.googleusercontent.com/search?q=cache:k4NSoCLQvyMJ:https://orbex.space/assets/uploads/documents/Orbex-TPA2018-Job-Specification.pdfPressure feds have some attractions for upper stages. OTOH 3.5tonnes is well over the line where turbo machinery is a good choice (rather than reciprocating pumps)It is and you're right. Orbex has been recruiting Turbomachinery engineers for years, and I have it on good authority that they've recently "finished" their assembly- at least to the point where they're ready to begin testing.Firstly welcome to the site. I think what's impressed various posters is the claim on the Orbex website of a 7.5Kg engine that can lift a 3.5tonne stage. which is phenomenal . Even with the the ability to run a very large nozzle on an upper stage due to near vacuum exhaust conditions, that's still very big, in fact it's a T/W ratio of 466:1Can you shed any light on this apparent paradox?
Hey thanks! I spend so much time lurking here figured it was time to make an account. Not sure about that claim. But the image they use next to the 7.5 kg figure is their 2nd stage engine...so maybe a 7.5 kg engine can propel 3.5 tonnes...in microgravity? That, or the first stage engine's actually 75 kg!
While our home spaceport at Sutherland moves rapidly ahead, we're busy building the launch vehicle. This is a full-scale main stage mandrel for Europe's 1st linerless carbon fibre LOX tanks, a technology we spent 4 years developing in-house with support from @H2020SME @spacegovuk
Presser: · Orbex is 1st UK space-sector company to win prestigious Horizon 2020 fundingThe funding round is completed by a €2.5 million grant from the European Horizon 2020 SME Instrument programme – the first for a UK space-sector company – to support the development of patented coaxial tanking technology. Orbex previously won £5.5 million in grant funding from the UK Space Agency’s Launch UK programme in 2018.
AFAIK, because the UK is leaving the EU, they can't participate any longer.
The CEO of Scottish rocket company Orbex, Chris Larmour, praised the ruling, saying it was good news for both the UK’s space sector and the local economy.“This is extremely positive news for a wide variety of communities and businesses and paves the way for the Pathfinder launch of small satellites from Sutherland Spaceport in Scotland.“We’re especially pleased for the crofters of the Melness Crofters Estate, who will be able to protect and develop their community with modern jobs. Sutherland is still the only UK spaceport with planning permission and now, with this ruling, the countdown to space launch from the UK can begin.”
Rocket builder takes on more space for its growing Forres workforce Rocket builder Orbex is expanding its operations in Moray, with a move into a building close to its headquarters.The company’s chief executive, Chris Larmour, said it needed the extra space to accommodate its growing workforce and house new equipment.The firm is also working on a detailed planning application for a new factory that could create hundreds of new jobs.Orbex, which is aiming to start launching its Prime mini-satellite carrying rockets from the planned Space Hub Sutherland spaceport next year, opened its base on Forres Enterprise Park in 2019.