nickjarboe
Joined 12 years ago
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Joined 12 years ago
I was mostly just correcting your "one-sixteenth of the energy required for orbit" statement. I agree that reentering at 7.8 km/s is much more difficult than 2.0 km/s, but the second stage is smaller and more spherical than the first stage. That might make reentering it a bit easier than if it had the shape of the first stage.
Just look at how much larger the first stage (mass almost all propellant) is compared to the second stage (large fraction of the mass is the payload).
[1] https://en.wikipedia.org/wiki/Tsiolkovsky_rocket_equation
[1]https://www.nature.com/nature/journal/v544/n7651/full/nature...