One of the problems with space flight is the speed required to achieve orbit; 17,500 mph. One of the ways I've always thought to achieve this was to launch at a low speed intoto a very high altitude then let the rocket fall back to earth, being speed up by the gravity until it reaches orbitalorbital velocity and begins orbiting.
Question: Are theirthere any programmes for this by the major space agencies, or papers written about the practicality of it?