RE: [amsat-bb] satellite propulsion thrust equations

["Reicher, James" <JReicher@xxxxxxxxxxx>]

Now I'm no rocket scientist, but AO7 travels in an orbit at around 900
miles (1500 KM).  It's been up there for over 30 years and has a decent
footprint, enough so that it's possible to work Europe from here in the
Great Blackhole of the Midwest.  Why is it not possible to send more
satellites into a similar orbit?

73 de N8AU, Jim in Raymore, MO


-----Original Message-----
From: owner-AMSAT-BB@amsat.org [mailto:owner-AMSAT-BB@amsat.org] On
Behalf Of Andrew Glasbrenner
Sent: Tuesday, October 11, 2005 5:37 PM
To: G0MRF@aol.com; amsat-bb@amsat.org
Subject: Re: [amsat-bb] satellite propulsion thrust equations

Just for giggles, here is a very similar concept. I notice they are on C
and S band. I wonder what the sats that made it up are doing now that
the rest of the constellation has been cancelled....

http://www.skyrocket.de/space/doc_sdat/ico.htm

73, Drew KO4MA

-----Original Message-----
From: G0MRF@aol.com
Sent: Oct 11, 2005 5:31 PM
To: amsat-bb@amsat.org
Subject: [amsat-bb] satellite propulsion thrust equations

Ooops  forgot the .co.uk
 
_http://www.g0mrf.freeserve.co.uk/MEOSAT.htm_ 
(http://www.g0mrf.freeserve.co.uk/MEOSAT.htm) 
 
David
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