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Assembling the BPM 5 - Bipropellant rocket engine

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Copenhagen Suborbitals

Copenhagen Suborbitals

Күн бұрын

Пікірлер: 67
@larryrosa6246
@larryrosa6246 6 жыл бұрын
Great !, the first time i have ever seen a assembly manual live for a bipropellant rocket engine .
@fomalhaut86
@fomalhaut86 5 жыл бұрын
You do show a lot of Your technology. Today most people won't disclose anything that might have any value. I'm impressed.
@cams1365
@cams1365 5 жыл бұрын
They're a non-profit organization.
@BigCroca
@BigCroca 5 жыл бұрын
they work for free so i guess showing their technology encourages donor's and backers.
@johndododoe1411
@johndododoe1411 2 жыл бұрын
The only details they hide are the ones NATO want to keep secret. The governments don't want this engine copied into a Palestinian missile.
@gym_bob
@gym_bob 5 жыл бұрын
I really admire what you guys are doing....Good luck
@justiceanddevelopments873
@justiceanddevelopments873 4 жыл бұрын
You’re Great Brother. Because of you now we learn rocket science ❣️
@meloirgrange2603
@meloirgrange2603 5 жыл бұрын
I love your mechanical parts. It s beautiful.
@omsingharjit
@omsingharjit Жыл бұрын
this video is recommended by my lucky click on the Play list after wondering how this part is done .
@rowlandreeves5476
@rowlandreeves5476 2 жыл бұрын
Thank you. Well done and very understandable by a novice like me.
@BushCampingTools
@BushCampingTools 8 жыл бұрын
Ok at 7:38 u answer the question I was going to ask re approaching the boiling point. Fantastic video, great work!!
@almosthuman4457
@almosthuman4457 4 жыл бұрын
those welds are terrifying for a rocket engine.
@CopenhagenSuborbitals
@CopenhagenSuborbitals 4 жыл бұрын
This was more or less a pathfinder, we later got better and better with our production methods and quality. Nonetheless, even with trying we didn't manage to reach the breaking point of this engine.
@talon0863
@talon0863 9 жыл бұрын
Thank you. Very well explained. I look forward to the next Video. Beautiful work!
@excellenceinanimation960
@excellenceinanimation960 Жыл бұрын
Amazing!
@cappnzak
@cappnzak 9 жыл бұрын
Excellent! Thank you. Great explanations.
@omsingharjit
@omsingharjit Жыл бұрын
I am wondering , if it also done by 3d Additive Type printers or by Casting and plating methods?
@ChongMcBong
@ChongMcBong 9 жыл бұрын
very nice design, looking forward to seeing it fly :)
@carlosalbertovelascoquirog9957
@carlosalbertovelascoquirog9957 3 жыл бұрын
Buen trabajo... Son una motivación para seguir adelante
@IDoNotLikeHandlesOnYT
@IDoNotLikeHandlesOnYT 4 жыл бұрын
The idea of tuning the cooling by shaping the wires is interesting. Has any other engine used that method?
@stephenstudley185
@stephenstudley185 5 жыл бұрын
I'm wondering if your design will scale down for use in model rocketry? I would love to use this design to go 10-20k, likely beyond my budget. I'd love to find out!
@cristianacosta7837
@cristianacosta7837 7 жыл бұрын
I have a question. What is the material of the manifold, inner and outer liner? Thanks.
@alphastronghold4425
@alphastronghold4425 4 жыл бұрын
In a past video was cited Stainless Steel.
@dan445678
@dan445678 6 жыл бұрын
I believe this is an outdated design for you all, but I did have a question about cooling. From what I understand would you not want the fuel to spend as little time in the cooling chamber as possible? In order to maintain the highest possible temperature differential. Of course this would also be dependent on mass flow rate due to total heat capacity of the fuel when thinking about it as a control volume. But yeah you mentioned you want the fuel to stay in the cooling jacket for longer, but I was under the impression you'd want the opposite.
@Rasmus0909
@Rasmus0909 6 жыл бұрын
You want the fuel to heat as much as possible and the chamber wall to be as cool as possible. These two contradict eachother and you need to choose a middle ground.
@taylorinase8094
@taylorinase8094 5 жыл бұрын
So many 90 degree angles, the regenerative geometry makes me nervous. Many other components are awesome
@mode1charlie170
@mode1charlie170 6 жыл бұрын
I have never seen a rocket engine with a combustion chamber so long. Just wondering why... is there a heat transfer issue? The equations that dictate chamber volume don't agree with a chamber of that size.
@Orandu
@Orandu 5 жыл бұрын
Dean Shaw I don’t know for sure, but I think it’s because of the low pressure on the feed side.
@hybriddyneguy
@hybriddyneguy 9 жыл бұрын
I like the Ball Valve design, Typically the H2o2 valves operate the same way. Does your injector design offer Boundary Layer Cooling? I thought I saw some alcohol injectors towards the outer edges.
@PyroShim
@PyroShim 9 жыл бұрын
Isn't the thermal conductivity of oxygen higher than that of alcohol? Also the oxygen would expand as it is heated, which would compensate for the pressure loss in the system.
@souravsinha7689
@souravsinha7689 6 жыл бұрын
liquid oxygen would oxidise(burn ) the hot metal
@bandiras2
@bandiras2 9 жыл бұрын
Re: PyroShim They need liquid oxygen to inject, becouse the injector design reqie liquid to operate properly. I think. High tech russian engines can use overheated oxygen gas, but that design is completly different than this.
@fernandohood5542
@fernandohood5542 4 жыл бұрын
The injector part is a tad bit unclear.
@CopenhagenSuborbitals
@CopenhagenSuborbitals 4 жыл бұрын
Although it's a different injector design, but perhaps this video is a bit clearer: kzfaq.info/get/bejne/ZtemldydnLHZfqs.html
@fernandohood5542
@fernandohood5542 4 жыл бұрын
@@CopenhagenSuborbitals Yes that one makes things much clearer.
@ethingeorge4450
@ethingeorge4450 3 жыл бұрын
Hi... can you make a video on PMD tank design specially on Cryogenic fuel
@brotherhoodofgamers8686
@brotherhoodofgamers8686 6 жыл бұрын
Make a video on how you make it like for instance what do you do to make the nozzle
@CopenhagenSuborbitals
@CopenhagenSuborbitals 6 жыл бұрын
Brotherhood of Gamers we have showed most of the production in various videos. Surf around our channel :-)
@manishd3590
@manishd3590 4 жыл бұрын
How do you make those injector channels? I have been trying to know it for a long time
@johndododoe1411
@johndododoe1411 2 жыл бұрын
The 0.9mm injection holes are drilled one by one. The larger holes are also simply drilled. They have mentioned that every time a drilling is slightly wrong, they need to throw away the steel object and make a new one. For their new BPM-100 engine they use prefabricated injector nozzles mounted in s plate with larger holes.
@Graham.556
@Graham.556 5 жыл бұрын
Very good engine what are the stats? ISP, Thrust,?
@johndododoe1411
@johndododoe1411 2 жыл бұрын
5 kN thrust design. They have a training project to double that while the senior team works on the 100 kN engine.
@tristanlongangue5671
@tristanlongangue5671 2 жыл бұрын
How heavy is a bpm engine?
@oak4901
@oak4901 6 жыл бұрын
does not the valve motor weigh as much as second valve? Good explanation otherwise...
@StormSilvawalker
@StormSilvawalker 7 жыл бұрын
what if you launched this as a rockoon?
@GamingMetNick
@GamingMetNick 6 жыл бұрын
Storm Silvawalker not gonna work
@inex4431
@inex4431 4 жыл бұрын
Wish I could help... :( dont have materials to though
@BigCroca
@BigCroca 5 жыл бұрын
hey can i fly in the rocket? i weigh 110 - 115 it would go higher with me! ;) XD
@justanotherasian4395
@justanotherasian4395 5 жыл бұрын
Sure if you can buy your own parachute
@omsingharjit
@omsingharjit Жыл бұрын
No Guarantee for your safe landing . Lol😂
@user-xs7hd3xp3u
@user-xs7hd3xp3u 7 жыл бұрын
我是用石墨的
@titter3648
@titter3648 8 жыл бұрын
Seems a little amateur like to me. Bad quality welds, no deburring of the holes, rough machining, and apparently does not know about pneumatic regulation valves that is a whole lot faster and a lot more precise than just putting a servo on a normal valve and messing a little with the ball hole (as oppose to the proper seat on a proper regulation valve). And how is fuel pumped on this rocket? Fuel flow could be regulated by the pump in stead of the valve.
@quevicular
@quevicular 7 жыл бұрын
fuk man, the welds are attrocious, lmfao. Just horrible to say the least. can you say BOOOOM!!!!
@sycodeathman
@sycodeathman 7 жыл бұрын
Fuel flow is determined by tank pressure; the tanks are pressurized with nitrogen (or some other inert gas) to a level that will force fuel out of the tanks at whatever rate they've designed for. That fuel then flows through the engine plumbing and into the combustion chamber. This method of moving fuel in a rocket is called a 'blow down' pressure fed system, which results in low combustion chamber pressure and correlated low thrust, but is simple as far as liquid rockets go and is good for rockets that are designed to be as cheap and as simple as possible.
@Anvilshock
@Anvilshock 7 жыл бұрын
Part of the leaning process, I'd say.
@faizantariq6595
@faizantariq6595 6 жыл бұрын
Wankel Motor why don't you make a perfect one????
@CopenhagenSuborbitals
@CopenhagenSuborbitals 6 жыл бұрын
ChiefJustice Middleton we call it the FrankenEngine because of that. This was the first engine, where we had to learn a lot
@jaratt85
@jaratt85 5 жыл бұрын
Sorry to say but whoever is doing your welding needs to go back to school.. those wouldn't pass any welding certification for pressure in the US.
@johnfrancisdoe1563
@johnfrancisdoe1563 5 жыл бұрын
J.A.Ratt85 They pressure test the assembly.
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