LIQUID PROPELLANT ROCKET ENGINE/liquid rocket 3d animation/construction working/ LEARN FROM THE BASE

Very nice,

you made a typo you said turbo pumb its spelled pump

Please teach me animation

Very nice

I fully understand with 3D animation
Great job! And keep going 🫡

Please 🙏 I need 3d animation

xydizer is liqued oxygen and propelant is kerosine. Ok?

Hello what software did you use for 3d animation of this rocket? Thank you!

I became your big fan

Nice video

Its wild to think of how far fuel injection has came on cars, motorcycles, small engines in general, and to see the same principles being applied at this scale is incredible.

Working principle Looks very simple in comparison to a car engine.

Can you please make an animated video on nuclear rocket engine

🇺🇸США-Европа блок НАТО Великая держава ✊✊✊

А Россия етих система скрывает как крисанути

👍

Please explain the working principle of helicopter

Why the space shuttle solid rocket booster?

Missile engine,,cruise misile

Can you make a 3d animation video about General theory of relativity?

The another dout is this, what is oxidizer and what is difference between oxygen and oxidizer

I have an another dout

My dout is this, how the liquid hydrogen and oxidizer is push to turbopump

I have an dout

sir for animation which software/ app you use? please can you tell me?

Awesome video can you make a video How hypersonic engine works many thanks

Transport phenomena

Very nice video . Good information given In this video

Bruhhhh what da hell that ain't a fuel tank that's a solid motor

Thanks sir 🥰

Super hit

give raction for oxidizer

Where is Oxidize and Fuel Pump?

fuel oxidizer

Thankyou sir

Thrust is a function of the mass flow through the nozzle. A tiny rocket engine and a massive rocket engine with the same exit-to-throat area ratio will produce the same velocity exhaust under the same conditions, but the massive rocket engine will be moving much more mass at that same velocity due to increase in volume at the throat. Based on your statement about thrust being a function of velocity, which we would relate to Mach number in this case, one would assume that the requirements of this systems thrust could be implemented by using a desired Mach number to find the desired area ratio. This would be nice, but unfortunately the area ratio equation proves transcendental when trying to solve for said ratio and can only be done through computer aided simulation, which does not give consistent data.

Liquid propellant is converted to solid state propellant on the fly.

awrsome information in the field of space

Hi. which app do you use to create this video i mean 3D and 360 photos and videos?

That’s a solid fuel booster lol. But still good explanation

I want to build a rocket. I'm an Engineering student. can anyone send me a model to mack it . Please.

топливо в ракете обычно искры не требует, когда топливо в стречает жидкий кислород оно просто анигилируется.

First of all the inside is hollow second of all it has its own solid fuel third of all it’s an SIDE BOOSTER

Big bang animation

This is a solid rocket motor not a liquid rocket they use this on the space shuttle it's solid fuel

Good concept but poor grammar. Made it difficult to follow.

Awsome and simple and clear explanation and animation..
Make video for cryogenic engines
And recent rockets like RLV TD, etc..

Please make animated video on galilean transformation of mechanics.

actually liquid rockets have the combustion chamber in the engine while for solid rockets the whole rocket is the combustion chamber which of course makes the whole rocket heavier .... the hull of solid rocket boosters is around 160 kg/m² or just around 100 kg/m² for the European P80 ... i

Got a job in isro