[amsat-bb] Re: New Cubesat - the Ultimate Fox Hunt
Jim Jerzycke
kq6ea at pacbell.net
Sun Aug 9 16:51:54 PDT 2009
Yeah, it might wind up being a super-sonic "Lawn Dart"!
Jim KQ6EA
--- On Sun, 8/9/09, G0MRF at aol.com <G0MRF at aol.com> wrote:
From: G0MRF at aol.com <G0MRF at aol.com>
Subject: [amsat-bb] Re: New Cubesat - the Ultimate Fox Hunt
To: bruninga at usna.edu
Cc: amsat-bb at amsat.org
Date: Sunday, August 9, 2009, 4:31 PM
In a message dated 09/08/2009 19:42:06 GMT Standard Time, nss at mwt.net
writes:
Why is it that all re-entries always end in the ball of fire over just a
few minutes. Why cannot the re-enetry energy be disipated over a longer
period to make it more survivable. Of course, if they could, they would. It
appears to be the nature of the beast. You are entering an ever denser
medium, so the drag has to escallate and you end up with the 6/7 minute burn.
>
>What if the surface of the re-entry vehicle radically changed during the
re-entry phase? As the density of the atomosphere increased, the surface
area decreases. An ablative system that instead of burning off a thin skin
of material as in most re-entry systems, you planned on burning off 95% of
the original drag volume? What re-entry profile could be achieved Could
we make a golfball core "pinger" that could survive?
Or, the not so 'cube'sat structure is an aerodynamic shape made from a cast
ceramic material which glides in at a shallow angle allowing the energy to
be dissipated over a much longer period of time.
OK the solar cells burn off but an internal antenna would be OK as ceramics
are fairly transparent to RF and a battery would provide the final hour or
so of tlm.
Would love to see the temp readings as it comes down.
Would not love to be on the final end of the trajectory when it arrives.
David G0MRF
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