This sounds a lot more like a transfer stage than a second stage. If this really were a second stage, there would have to be a very powerful single stage to orbit system to get payloads into orbit where they could join this stage to be lifted into GSO, the Moon or wherever. That seems hugely wasteful since it would require getting the entire first stage mass up to orbital speed.
Awhile ago, Elon Musk proposed that NASA should focus on really new ideas such as a nuclear powered Mars shuttle system. The idea is the same, use chemical rockets to get stuff into Low Earth Orbit, join up with the permanently orbiting nuclear "taxi" and let it power the payload anywhere in the Solar System. Launches using nuclear engines from the Earth's surface have some really terrifying problems, but once in space, they're a lot more reasonable.
Chemical rockets for deep space, e.g. Mars, seem pretty wimpy to me.
Awhile ago, Elon Musk proposed that NASA should focus on really new ideas such as a nuclear powered Mars shuttle system. The idea is the same, use chemical rockets to get stuff into Low Earth Orbit, join up with the permanently orbiting nuclear "taxi" and let it power the payload anywhere in the Solar System. Launches using nuclear engines from the Earth's surface have some really terrifying problems, but once in space, they're a lot more reasonable.
Chemical rockets for deep space, e.g. Mars, seem pretty wimpy to me.