Point 1: Rockets ranging from gross mass of 100Kg to 1000Kg are capable of orbital insertion. (Microlaunchers)
Point 2: DIY space explorers must aim for > LEO due to the fact that LEO is crowded, regulated, and a little boring by now (my paraphrase).
Point 3: For microlaunchers, atmospheric drag becomes significant.
To point 3, I wonder if a launch from high altitude balloon(s) would get us up faster. Any comments or suggestions?
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A rockoon was also an entry into the X Prize that produced SpaceShipOne.
Bigger projects for avoiding the atmosphere:
https://en.wikipedia.org/wiki/StarTram
https://en.wikipedia.org/wiki/Launch_loop
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