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Old 08-14-2021, 12:46 PM   #1 (permalink)
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The Genius of 3D Printed Rockets

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The Genius of 3D Printed Rockets




Why am I posting this on ecomodder...???

Well, it is transportation oriented...

Manufacturing eco also....

And...

I think it’s pretty cool...😎





>

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Disclaimer...

I’m not a climatologist, aerodynamicist, virologist, physicist, astrodynamicist or marine biologist..

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I play one on the internet.

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Old 08-14-2021, 01:25 PM   #2 (permalink)
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When I saw the title, I thought it would be about Integza. I've been following his experiments with vortex hybrid rockets and 3D printed solid fuel. The latest:


_______________

I watched the video. That kid is the founder of the company?!?


edit: If you want something to make you think more, try Sabin-a Hossenfelder: Physicist Despairs over Vacuum Energy
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Old 08-15-2021, 02:42 PM   #3 (permalink)
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Depending on thrust and oxidizer requirements, fuel can be just about anything. Printing it is odd, but why not? Easier/faster to use the motor tube as a form and a center insert for burn formation, however. Unless you drop it.
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Old 08-16-2021, 11:59 AM   #4 (permalink)
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They'll have a big second-mover advantage WRT reusable launch vehicles vs SpaceX.

I also like that their production easily scales in a linear fashion... add more machines, build more in parallel. But at the same time, they won't enjoy the economies of scale SpaceX can do. He even mentions this in the video. I wonder what the failure rate for their "one big part" is vs traditional methods... like, porous spots in the print, etc?

Sam
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Old 08-16-2021, 01:54 PM   #5 (permalink)
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IMHO if they get the first layer to stick they're half the way there.
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Old 08-16-2021, 02:47 PM   #6 (permalink)
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Quote:
Originally Posted by samwichse View Post
I wonder what the failure rate for their "one big part" is vs traditional methods... like, porous spots in the print, etc?

Sam
Probably the same for the solids on the shuttle, statistically 1 failure per 100 launches.*

Porous just makes the burn accelerate in odd ways and can lead to skin burn throughs: so boom , too much thrust, not enough thrust, asymmetric thrust, whatever.
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Old 08-16-2021, 04:07 PM   #7 (permalink)
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I watched this last week and thought it was also very interesting. Being aerospace I'd imagine their quality control has to be pretty ridiculous. They probably x-ray these parts before anything is put in use or even tested.
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Old 08-16-2021, 06:07 PM   #8 (permalink)
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magna-flux: duckduckgo.com/?q=magna-flux&ia=web
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Old 08-16-2021, 08:38 PM   #9 (permalink)
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Fwiw, we did ultrasound only on the shuttle solid boosters, nitroglycerin mixed with aluminum chlorhydrate and a rubber binder/filler is a wee bit unstable to be putting much energy into. They did withstand rail and truck transport but not dropping

Since everyone was paranoid about propellant but not temps or o rings this kinda worked

Those were fun days.
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Old 08-18-2021, 10:47 AM   #10 (permalink)
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They mentioned a 10-15% (if I recall correctly) weight penalty. That seems significant to me, but perhaps its not for the rocket as a whole?

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