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To: RightWhale
The one satellite needn't have just a small antenna, nor even just one antenna.

Let's try a 'fer instance' using a relatively modern, more or less common example of what we're looking at here -

- let's take the NWS's WSR-88D which employs a 28' dish, an S-band freq of 2.4 GHz (thereabouts) which results in 45 dB of gain and a 3 dB beamwidth of just under a (1) degree ...

... do you know what kind of distance an arc of 1 degree covers at 35,786 kilometers (19,323 nautical miles or 22,241 statute miles) above the earth's surface?

The problem that arises is that - MULTIPLE 'targets' would be indicated with a beamwidth at that distance - and I've not consdered the path-loss that would be encountered *both* directions - with a poor reflection/reflector (the bogey aircraft) as the source for the return (signal) ...

A better solution might be increased use of land-based OTH (Over The Horizon) HF (High Frequency) RADAR rather than a) balloons or b) an impossible satellite solution ...

38 posted on 03/05/2004 5:35:16 PM PST by _Jim ( <--- Ann C. and Rush L. speak on gutless Liberals (RealAudio files))
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To: _Jim
That's just optics. There's no particular reason aside from not wanting to pay for the launch costs of having a huge antenna or antenna array at geosynch elevation. Even NASA is designing monstrous arrays for deployment in space so they can spot earthlike planets lightyears away, although the new mandate may have changed the schedule. But apertures can be synthesized. The actual size of the antenna isn't such a major factor so long as the antenna can pick up signal.
39 posted on 03/05/2004 5:44:33 PM PST by RightWhale (Theorems link concepts; proofs establish links)
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