I have, but that video has an error: it's not a hybrid rocket engine because a rocket by definition contains all of it's reaction mass. Meanwhile both a turbine and a scramjet use oxygen from the air which gets incorporated into the carbon dioxide and water molecules which fly out the exhaust nozzle to give the aircraft thrust.
A rocket would have two tanks: one would be a fuel tank carrying either hydrogen or kerosene while the other would contain the oxygen used to burn it.
A jet (whether it's a turbine or a ramjet) would only have a fuel tanks filled with kerosene and it would get the oxygen to burn it from the surrounding air.
A turbine engine uses the superheated gases used to provide thrust to turn a turbine at the front which sucks in the air (and oxygen) used to burn the fuel:
A ramjet uses the forward motion of the aircraft to push air into the engine to burn the fuel:
You can achieve higher speeds with a ramjet but you can't start it from a dead stop. A combined cycle has two reactors for each inlet. At lower speeds (less than Mach 3), the air will be directed to the turbine reactor while at speeds between Mach 3 and Mach 6, it will be directed to the ramjet: nextbigfuture.s3.amazonaws.com/.../...cengine.jpeg
So the turbo is sitting atop the ramjet? It's a simple engine, eh? Kerosene. So, does it use a gradually decreasing outlet in order to create more force like with liquid? Or does it not need this with concern to it being heated air?
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I have, but that video has an error: it's not a hybrid rocket engine because a rocket by definition contains all of it's reaction mass. Meanwhile both a turbine and a scramjet use oxygen from the air which gets incorporated into the carbon dioxide and water molecules which fly out the exhaust nozzle to give the aircraft thrust.
Tell us more.
A rocket would have two tanks: one would be a fuel tank carrying either hydrogen or kerosene while the other would contain the oxygen used to burn it.
![Have you heard of the SR-72?]()
![Have you heard of the SR-72?]()
A jet (whether it's a turbine or a ramjet) would only have a fuel tanks filled with kerosene and it would get the oxygen to burn it from the surrounding air.
A turbine engine uses the superheated gases used to provide thrust to turn a turbine at the front which sucks in the air (and oxygen) used to burn the fuel:
A ramjet uses the forward motion of the aircraft to push air into the engine to burn the fuel:
You can achieve higher speeds with a ramjet but you can't start it from a dead stop. A combined cycle has two reactors for each inlet. At lower speeds (less than Mach 3), the air will be directed to the turbine reactor while at speeds between Mach 3 and Mach 6, it will be directed to the ramjet:
nextbigfuture.s3.amazonaws.com/.../...cengine.jpeg
So the turbo is sitting atop the ramjet? It's a simple engine, eh? Kerosene. So, does it use a gradually decreasing outlet in order to create more force like with liquid? Or does it not need this with concern to it being heated air?
All the exhaust would be in the form of gas when it leaves the engine.
I am looking forward to seeing g the new F-47 but this is pretty amazing
I saw one on it as well. No pilot needed. It looks as tho it has anti gravity the way it moves.
At that speed. Seems like it could reach the space station!
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