In article <kk65dn$1jf$
1...@dont-email.me>,
bri...@blueyonder.co.uk
says...
>
> It occurs to me with this mission to move an asteroid and bring it into a
> different orbit closer to the moon/earth system,that there are possible
> dangers with this plan. Its got to be reasonably low in mass one supposes as
> it would not be very easy to move it, on the other hand all this talking
> about ion propulsion leads me to believe it will take a long tome to
> achieve much movement even on a light weight one.
> So if its too big and anything goes wrong it might become a hazared, and
> need a lot of power to move it, but too light and it will not really be
> worth mounting a manned mission there afterwards, not to mention if the
> moving craft is still attached it might be a hazard in itself.
Orbital mechanics is well understood. It's highly doubtful that the
mission would be designed in such a way that anything could go wrong.
Changes to the orbit would necessarily be made very slowly, with
observations made frequent enough that any danger would be avoided.
> This looks lie a bit of a back of the envelope idea to me.
To me this is a bit of a strange mission. It only makes sense to me if
there is to be a follow-on manned mission to the asteroid once it's in
an orbit much "closer" to the earth than its original orbit.
Still, I'm not sure the math works out. Unless there is some net
savings in cost somewhere, why not send a mission directly to the
asteroid in the first place?
Jeff
--
"the perennial claim that hypersonic airbreathing propulsion would
magically make space launch cheaper is nonsense -- LOX is much cheaper
than advanced airbreathing engines, and so are the tanks to put it in
and the extra thrust to carry it." - Henry Spencer