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|    Message 44,244 of 45,986    |
|    A Random Person to nu...@bid.nes    |
|    Re: Oxygen Fuel for Jupiter-air-breathin    |
|    14 Aug 16 22:23:54    |
      From: dos4004@gmail.com              On Sunday, August 14, 2016 at 7:57:56 PM UTC-7, nu...@bid.nes wrote:       > On Saturday, August 13, 2016 at 10:44:25 PM UTC-7, A Random Person wrote:       > > If Jupiter's atmosphere is 90% H2, then would it make sense to use a       > > turbojet/ramjet/scramjet with Oxygen (or some other oxidiser) as fuel? How       > > would its efficiency compare with that of conventional airbreathing       engines?       >        > Fun idea!       >        > Hydrogen-fueled jet aircraft have been proposed for use in our atmosphere,       and AIUI the efficiency is about equal, given the different tankage       requirements and having to keep the hydrogen cold enough to make it dense       enough to get energy density        equivalent to conventional jet fuels.       >        > A Jupiter-air-breathing jet would need liquid oxygen tanks, and would need       to move fast enough to gather hydrogen rapidly enough to stay aloft, meaning       altitude limits. Of course once the O2 runs out it's a glider and there's       nowhere to land.       >        > Fluorine is a better oxidizer so you'd get more runtime than with oxygen,       but the "exhaust" is hydrogen fluoride, and if there's anything alive in       Jupiter's atmosphere it won't like that, not to mention the technical       challenges of keeping the engine        from dissolving- HF is VERY chemically reactive.       >        > So, how about a Jupiter-air-breathing engine of some sort powering the       instrument package on a Jupiter balloon probe? It'd be cheaper than a nuke       generator and could be restartable so it wouldn't have to run constantly.       >        > Another challenge; at the depth in Jupiter's atmosphere where the air       pressure is equivalent to Earth's at sea level, the temperature is ~ -100C and       you're in the ammonium-hydrosulfide clouds. When you go deep enough for what       we think of as        shirtsleeve temperatures you're back in mostly hydrogen but the pressure is ~       5-10 Earth atmospheres. So, whatever engine you choose, it won't work quite       the same way it would on Earth.       >        >        > Mark L. Fergerson              Thanks!       Originally I was wondering how usable it would be as a Jupiter SSTO, but I see       now it would make more sense to use some kind of nuclear engine.              --- SoupGate-Win32 v1.05        * Origin: you cannot sedate... all the things you hate (1:229/2)    |
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