- #1
paul3337
- 5
- 0
I heard of a strange engineering concept that was mentioned to me by someone who claimed to be a retired aerospace engineer. It was a guy I met on the internet so I took what he said to me with huge grain of salt.
He said something to me that I barely comprehend and I haven't heard from this guy in a year or so but it has got me curious to ask about it here.
This guy stated one time that if you were to ionize the atmosphere on the nose of a missile, or possibly the nose of an aircraft such as that one passenger jet that was once used that could fly faster than the speed of sound, that it would create a sheath of plasma that would reduce drag and enable a missile or an aircraft to go beyond mach 10 without overheating or breaking up.
I call nonsense on this but curiosity has gotten the better of me and now I got to ask:
Is there something to what he said?
If so, if SpaceX somehow ionized the atmosphere off the nose of the first stage of their rocket ship/superheavy vehicle, would it reduce drag? If so, would that lead to better fuel efficiency for the sea level raptor engines?
I just thought it would be wise to ask about it on a forum like this before completely discarding the idea. :)
He said something to me that I barely comprehend and I haven't heard from this guy in a year or so but it has got me curious to ask about it here.
This guy stated one time that if you were to ionize the atmosphere on the nose of a missile, or possibly the nose of an aircraft such as that one passenger jet that was once used that could fly faster than the speed of sound, that it would create a sheath of plasma that would reduce drag and enable a missile or an aircraft to go beyond mach 10 without overheating or breaking up.
I call nonsense on this but curiosity has gotten the better of me and now I got to ask:
Is there something to what he said?
If so, if SpaceX somehow ionized the atmosphere off the nose of the first stage of their rocket ship/superheavy vehicle, would it reduce drag? If so, would that lead to better fuel efficiency for the sea level raptor engines?
I just thought it would be wise to ask about it on a forum like this before completely discarding the idea. :)