- Jun 18, 2014
 
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"g. The exit point of the typical space elevator concept is at geostationary orbital altitude - some 22,000 miles above the equator. An object in orbit, and the exit point of the space elevator (at that altitude) would have a velocity of something like 3,400 miles per hour - far less than escape velocity. Maintaining a lower orbit (like that of ISS) requires much higher velocity (~17,000 mph); perhaps that is the cause of confusion."Here are some explanations:
To me this is the REAL fly in the ointment. The tendency of the mass at each orbital level will be trying to move at a different velocity. The sideways stresses would be enormous. Those stresses only zero out at the geosynchronous level, and would be a constant sideways force at every other level permanently.
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