posted on Jan, 13 2016 @ 02:36 PM
Thanks Sammishan, that's what I was looking for. Target uncertainty is a good point.
I'm not convinced on the cheaper or longer range part. I think it would have to be as large as a ballistic missile for the same range & payload at
least---the launch phase is the same for both.
How I see it: as the glide vehicle is unpowered, and all initial kinetic energy is supplied by the rocket booster in both cases, I don't see how you
could possibly get better range when you travel in a drag inducing atmosphere for a distance compared to a ballistic warhead which travels in a drag
inducing atmosphere for the minimum time possible for this reason.
If you want range, in both cases you need to get out of the dense atmosphere, and launch detectability is the same. For both, the necessary
trajectory is first up (get out of densest air quickly) and then sideways (to gain transverse velocity and hence range).
edit on 13-1-2016 by mbkennel because: (no reason given)
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edit on 13-1-2016 by mbkennel because: (no reason given)
edit on 13-1-2016 by mbkennel because: (no reason
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