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RE: satellite propulsion thrust equations



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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