Can you launch a rocket into space with a centrifuge?

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Lord Rory Gin

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Well, maybe. The theory is there and a scale downed version of the system has been built to accelerate a rocket to Mach+ but this company hopes to create a full size (1m diameter) rocket with an upper stage rocket motor and 200 kg payload so that they can launch into orbit for a fraction of the cost of other companies like Rocket Lab. To do this they intend to launch the rocket to Mach 7 and essentially replace a booster rocket and all its associated fuel with a centrifugal launcher. This video is a year old already so if anyone has an update regarding their progress, please post.
 
Alright, thanks. I should have figured that this was previously posted. But it doesn't appear that any updates have been posted on their progress. I did find one article from February that suggests that full size version is still in the works. It has more information on the 1/3 size prototype that has run at 20% speed and has launched 10 projectiles. I think the technology may eventually work but I'm not sure if it is financially viable - I mean, how many companies out there need to launch a 200-400 kg to space where a more conventional multi-stage rocket can do it.
https://newspaceeconomy.ca/2024/02/12/spinlaunch-company-profile/


Mods: please delete this thread or merge with the other thread. Thanks.
 
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Mach 7, huh? That's almost 8,000 feet per second. A=v^2/r Let's say you build one of things out of unobtanium, and it's 400 feet across, for a radius of 200 feet. That's 320,000 ft/sec^2, or 10,000 g's. Has there ever been a rocket that could stand 10,000 g's sideways? Or even 1,000? Is there a form of unobtainium that also works as rocket fuel? That this proposal hasn't been laughed out of every venue it's been mentioned at is an indictment of how physics is taught (or not taught) in the USA.

On the other hand, if you had something useful that could stand 100 g's (almost conceivable) maybe you could make a straight track somewhere, 2 miles long, that could obtain that speed with less trouble. You'd need the right mountain, I suppose. that still leaves a few problems, though. Even if it released at 15,000 feet, max q would still be, unless I've messed it up using internet calculators, on the order of 47,000 lbs/ft^2! That's as opposed to maybe 735 lbs for a Falcon 9, which would be something like 10 miles up and a bit over Mach 2. I'm sure there will be thermal issues, too, although I suppose if you made much of your vehicle out of uranium, that would be refractory enough. So it might be a valid way to deliver fissile material to orbit. I'm not sure anything short of large scale interplanetary exploration a la the Orion Project would need that much. And there just MIGHT be PR problems. I suppose if you were leaving the solar system, you could keep it all secret somehow until just after you left.

https://www.digitaldutch.com/atmoscalc/
http://www-mdp.eng.cam.ac.uk/web/library/enginfo/aerothermal_dvd_only/aero/compressible/index.html
https://www.flyingmag.com/has-anybo...ring a typical Falcon 9,or so into the flight.
 
You can launch a centrifuge into space with a rocket.

storm GIF
 
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