Are Ionospheric Scramjets possible?

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The discussion explores the feasibility of using scramjets in the ionosphere, specifically at altitudes around 100 km, where the air is extremely thin. While scramjets can theoretically reach speeds of Mach 25, which is near orbital velocity, the low density of oxygen in the ionosphere poses significant challenges for lift and thrust. At such high speeds, the limited amount of oxygen available may not provide sufficient fuel for combustion, raising questions about the viability of sustained flight. Additionally, even without drag, the thin atmosphere complicates the operation of scramjets. Ultimately, the concept remains largely theoretical due to the extreme conditions and limitations present at those altitudes.
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I was doing some Wikipedia browsing, and I came across the concept of Scramjets for spaceplanes. The highest estimate for a top speed of a scramjet in atmosphere is Mach 25, which is approximately orbital velocity. The ionosphere contains high levels of O, so would it be possible to fly a scramjet aircraft in it (at approx. 100km)?
 
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High fraction does not mean high amount - the ionosphere is extremely thin. You don't get much oxygen there, and not much lift. You need a very high speed to counter this. 100km is at the Kármán line, where the required flight speed reaches the orbital speed - your "plane" becomes a satellite.
 
Thanks. Thing is that at Mach 25, surely even though it is very thin, you are taking in some? Do you know if such a scramjet would work, even if it had very low thrust? And for the sake of the theory, assume that there is no drag.
 
I'm sure you can burn something, but airplanes are always a quantitative problem.
The air is thin, but at that speed drag is relevant.
 
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