Wondering what the best carbon allotrope to refuel rockets at Venus is.
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Replying to @andrewdoull @nyrath
Carbon monoxide/oxygen makes a good fuel/oxidizer combo. Gonna rest the technology on Mars in 2020 if this shutdown ever ends.
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The Isp though leads to challenging mass ratios.
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Not as bad as you might think! Isp is over 300s with a pumpfed vacuum engine, which is better than Earth sea level with most propellants. Density is good, and it actually takes significantly less energy to produce than higher Isp propellants. It’s OPTIMAL for Mars orbit, in fact.
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Replying to @Robotbeat @ToughSf and
If you are energy-limited (as you usually are w/ ISRU propellants), then you need to be careful not to pick a propellant with too high exhaust velocity (Isp). So a low Isp propellant can actually be MORE energy efficient than a hi Isp one. A counterintuitive result often ignored.
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+1 Most don't realize the economics become radically different than those of launching propellant out of earth's gravity well.
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