Mithras
Banded Mongoose
Hi, in my attempt to create an interesting solar system campaign using fusion rockets or nuclear thermal rockets, I need to design a hydrogen fuel scoop ship. This will scoop hydrogen from Saturns upper atmosphere. What kind of problems or solutions do you think I should be aware of? Clarke posits scooping from Titans atmosphere in Imperial Earth, but Saturns escape velocity is around 35kms. Saturns winds are the fastest in the solar system, exceeding 1500kmh.
I was considering a 200ton nuclear thermal rocket, streamlined.
Any idea what escape velocity i'd ned to consider? The full 35kmh, or would I shave some off that by being in the upper atmosphere, and not starting my return journey from the surface.
Thanks!
I was considering a 200ton nuclear thermal rocket, streamlined.
Any idea what escape velocity i'd ned to consider? The full 35kmh, or would I shave some off that by being in the upper atmosphere, and not starting my return journey from the surface.
Thanks!