Doesn't that completely depend on the thickness and material of the walls of the spacecraft? I.e., isn't it just a question of making the walls thick enough?
Doesn't that completely depend on the thickness and material of the walls of the spacecraft? I.e., isn't it just a question of making the walls thick enough?
The problem with shielding is the weight involved to achieve any level of protection.. wrapping the ship in enough lead to make a difference would be hard to get it off the ground. Also while this type of shielding may be effective against normal solar radiation, high energy galactic cosmic rays are far more dangerous and are almost unaffected by conventional shielding.
If you're interested, I recommend this paper. It goes a bit deeper into exactly why radiation is such a problem for any proposed Mars missions (warning, PDF):
http://spaceradiation.usra.edu/references/Ch4RadCarcinogen.p...
What happens to your Mars departure window when the rocket carrying your life support system goes off course and is destroyed by the range safety officer?
http://www.thespacereview.com/article/308/1
I hope this technology is thoroughly investigated before moving forward with the standard absorption method of radiation protection.
Whole body doses of 1 to 2 mSv/day accumulate in interplanetary space, and
approximately half of this value accumulates on planetary surfaces (Cucinotta et
al., 2006; NCRP, 2006).
That's millisieverts per day, not sieverts. Am I missing something?NASA has been making progress in making astronauts less susceptible to radiation damage through diet and vitamins. There's also this paper which talks about a vaccine that's being tested to counteract some of the body's responses to radiation exposure (PDF):
http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/2007002...