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Can somebody find me anything on this? I'm not good with the mathematics of this, so something that would give me the launch date, travel time, landing time, Mars lift-off time, and Earth return time would be good. You can assume that the rocket used to launch the mission has twice the power of the OTL Saturn V, and that the return stage to Earth has twice the power of the OTL S-IVB. Assume that the spacecraft weight is equal to double OTL's Apollo CM and SM combined, plus 100,000 pounds for the crew's living space and supplies.

Note: These numbers are based upon some really quick research, as I haven't got any of my notes with me.
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