where are you now man? you just disappeared from the internet
@Caliper_Click3 ай бұрын
What's its thrust?
@matiasren828835 ай бұрын
Does the engine have a throat and nozzle or is it just a flat hole and that's it?
@physics36326 ай бұрын
Amazing! I hope I get there too some day. For now I’m just trying to get pulse detonation engines to work well with injectors. What will your next steps with your engine be? Also how are you burning the alcohol in the engine? Are you just spraying it into the combustion chamber using a pump? Have you considered other fuels asides from ethanol? From my experience using diesel Or kerosene makes significantly more thrust over ethanol.
@ptrkmr7 ай бұрын
Those shock diamonds had me drooling
@ALRFEOA7 ай бұрын
Now we'll use that little rocket engine as rcs)))
@harleygreene13457 ай бұрын
Sporadic ignition source
@RealLostmatter7 ай бұрын
wow!
@MiguelAngel-bf4tc9 ай бұрын
Oigan que combustible tienes
@BigDickMark Жыл бұрын
Nice work guys!
@doalgodoo5832 Жыл бұрын
Awesome! how much does the engine weigh when removed from the supporting plate?
@nejcjug7135 Жыл бұрын
how thick is this coper engine
@leepalmer1210 Жыл бұрын
Why did it look like nearly all the fuel was wasted? It only ignited after it puked several liters of fuel. Is it due to the time it takes to get fuel vapor atomized in the chamber before ignition?
@fullflowaerospace2 жыл бұрын
nice!
@ok-hd4so2 жыл бұрын
the fuel igniting looks badass
@gustverschelde96542 жыл бұрын
does it has thrust?
@Vatsyayana87 Жыл бұрын
Any fluid moving out of a vessel has thrust.
@oneistar66612 жыл бұрын
Hey heyyyyy, either you're hijacked by Russians or have started good rocket engineering job. Just found you and need an update Space One.
@timoteomuniz34892 жыл бұрын
I've saw this before in other channel, how did you build it? Nice shock diamonds!
@stephonhaydes21662 жыл бұрын
I think test #31 was the most efficient....
@jake41862 жыл бұрын
Would you ever make a video showing the way everything works and how it works?
@user-sv9gn8xm7t2 жыл бұрын
Hi
@arnavkumar30602 жыл бұрын
It produces shock diamonds 😍😍😍
@FijiWater12272 жыл бұрын
What type of injector is it? It would be great if you can post cad files for the injector
@fehmidonmez78102 жыл бұрын
So what will be the thrust without any combustion? With just injector pressures. And thanks for that brief and quality video.
@tristanlongangue56712 жыл бұрын
Hey, how do you regulate the oxygen pressure?
@T112352 жыл бұрын
Are there any news or new videos? I'm interested in making a 50%alcool 50%water and oxigen engine but i don't know what are the challenges to make it
@matiasren82883Ай бұрын
Hey, water has very bad combustion. In fact, it is used to put out fires. You should do it with pressurized air, which, in addition to oxygen, has other elements that can burn.
@P4PYROIND2 жыл бұрын
All the best keep going ...✌️
@proto_hexagon56492 жыл бұрын
What is GOx?
@suryamani1235 Жыл бұрын
Gaseous Oxygen
@notmadrocketscientist19022 жыл бұрын
How do you manufacture the nozzle? Tube spinning? Forging?
@oneaerospace80222 жыл бұрын
By forging. So pretty similar to you if I remember correctly
@YTSeiyaGoFire2 жыл бұрын
Prob 1-5 kilonewtons of thrust
@rocketacademy45192 жыл бұрын
What nozel size are you using ( if you are using one )?
@oneaerospace80222 жыл бұрын
There was no combustion chamber and nozzle attached during this test. It was just a test of the injector, so the title is a little bit misleading. You can watch a test fire of the fully assembled rocket engine here: kzbin.info/www/bejne/Z5OUkoiHerSNnbc
@NOTTApro1422 жыл бұрын
It’s crazy how these make mach disks when the engines are so small. Maybe you could make a thrust calculator to see how much thrust these things produce
@oneaerospace80222 жыл бұрын
We directly measure the thrust on the test bench. It was a little over 11 N for this test. In a later test we increased the mass flow and reached 18 N.
@chr0my1342 жыл бұрын
more videos!
@oneaerospace80222 жыл бұрын
We have been working on some major modifications of our test stand and software recently. We will hopefully continue testing at the end of December or beginning of January. Stay tuned!
@SoberMustard2 жыл бұрын
I've seen those liquid spills somewhere on the internet
@skyloxsfs64023 жыл бұрын
How do you get test data
@oneaerospace80222 жыл бұрын
We use an arduino to aquire test data from all implemented sensors (pressure, temperature, thrust)
@jonahosterried78323 жыл бұрын
What has your fuel Flow been?
@oneaerospace80222 жыл бұрын
Fuel flow is given as total mass flow before every test in the video. Max was about 11 g/s
@kapytanhook3 жыл бұрын
So much chamber pressure, such nice mach diamonds but ISP of under 140. Makes the 400isp engines oit there seem even more impressive
@oneaerospace80222 жыл бұрын
They defenitely are! However, we can only reach very low chamber pressures of upt to 6.5 bar due to the pressure fed design approach. Thus, Isp is also very limited
@Wopictropic3 жыл бұрын
How are you mixing the ethanol and gox?
@oneaerospace80222 жыл бұрын
We use a coaxial swirl injector
@Wopictropic3 жыл бұрын
What is your Ethanol to Gox ratio?
@oneaerospace80222 жыл бұрын
O/F is ~1.0
@bigr35783 жыл бұрын
Where'd you get the oxidizer from?
@jpthepug31262 жыл бұрын
It’s just liquid oxygen I’m sure
@oneaerospace80222 жыл бұрын
We use gaseous oxygen from our local hardware store
@theredstonehive3 жыл бұрын
Nice mach diamonds
@JeffreyZhuang3 жыл бұрын
What is the diameter of the injector outlet?
@orbitalalpha94423 жыл бұрын
How do you make the combustion chamber and nozzle?
@sonha60773 жыл бұрын
Do rocket engine
@headbanger14283 жыл бұрын
I love pipe bomb 💣 rockets 🚀 especially when they do rapid unscheduled disassembly. No seriously, did you temper the steel before testing? I see cast iron, but I hope I’m wrong.
@tonyo9493 жыл бұрын
Very interesting project and results ! What is your injector and how do you build it ? And what is the pressure of GOx and Ethanol (how do you pressurize ethanol too ?) ?
@oneaerospace80223 жыл бұрын
Thank you! We use a coaxial swirl injector which is manufactured on a lathe. GOx pressure is around 10 bar and ethanol around 7 to 7.5. We use CO2 or nitrogen for the tank pressurization.
@melplishka59783 жыл бұрын
You got Mach diamonds happenin.
@ProMayvn3 жыл бұрын
Is it simply pressure fed? What pressures on your propellant and oxidizer are you using? This is so awesome!
@oneaerospace80223 жыл бұрын
Thank you! Yes, its simply pressure fed. The pressure on the ethanol side is 7 to 7.5 bar and around 10 bar for the oxygen.
@Muss_._3 жыл бұрын
hi.Im from Malaysia. After i watch your video about rocket,i very interested and i like it. I think i want make one but i dont know to make engine rocket hybrid. So, can u teach me how to make engine rocket? please