Nuclear Fusion Rockets v.s Fission

In summary, nuclear fusion rockets have the potential to reach 10% the speed of light, while nuclear fission rockets can only reach 5%. However, NASA is currently working on a spacecraft that can make a one-way trip from Earth to Mars in just two months, which is faster than the current six-month journey. This is due to the fact that light takes about 10 minutes to reach Mars, meaning that a fusion rocket could theoretically travel there at 10% the speed of light in just over 3 hours, including deceleration time. However, the reality is that current rocket technology does not allow for continuous acceleration and deceler
  • #36
you are basically saying its too complicated
 
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  • #37
It certainly is complicated.

I know this is one of Zubrin's ideas (http://www.npl.washington.edu/AV/altvw56.html) , but I'd have to review the details of his calculations, particularly the efficiency of the fission process.

It is very easy to consider Isp = vex/g, but is the vex based on the actual physics. If only the water is considered, then the calculation of Isp is incorrect. One must consider the presence of U and fission products in the stream. I would be interested in Zubrin's core design.

The other aspect is the materials degradation (corrosion/erosion) - which I suspect may not have been addressed.
 
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  • #38
actually i was thinking about that while I read your response yesterday, but i was unfuitful coming up with a fission chamber that would move up the rocket at the rate that metal errored away.
 
  • #39
Arian said:
actually i was thinking about that while I read your response yesterday, but i was unfuitful coming up with a fission chamber that would move up the rocket at the rate that metal errored away.
Well there is such a concept using Am-242m which undergoes spontaneous fission and has a reasonable fission cross-section. But the spontaneous fissioning is also a problem for handling and assembly. The spontaneous fission cannot be switched off and on - it is continuously on.

Erosion is a problem not only for fission systems, but any high temperature system, particularly where flow is involved.
 
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