134 karma · joined October 8, 2014
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...
[1]http://www.cnn.com/2016/03/23/politics/john-ehrlichman-richa...
Anderson: So what have all your creative people come up with, then? What’s different in your basic technology versus 50 years ago?
Musk: I can’t tell you much. We have essentially no patents in SpaceX. Our primary long-term competition is in China—if we published patents, it would be farcical, because the Chinese would just use them as a recipe book.
Also: reusable rockets.
This is, of course, a very simplified explanation. As one goes back hundreds of millions to billions of years, other large scale changes like plate tectonics, atmospheric composition/mass, sun brightness, continental weathering, etc. will cause the average surface temperature to vary considerably.
[1]http://www.mercerrestaurantgroup.com/how-to-open-a-restauran...