Revision as of 10:10, 3 July 2008 by Keithcu (talk | contribs)
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Here we will define the performance desired and the expected performance. This will help define what areas are most critical for development.

All values in this table need to re supported with as much information as possible.

Desired Expected
Payload mass 100 100
Max speed of ascent 1000 kph 200 kph
Time to GEO 1 day 1 week
Time to Moon 4 days 10 days
Time to Mars 1 month 3 months
Size limitations
Radiation load
Launches per year 365 200
Cost per kg to LEO $100 $1000
Cost per kg to GEO $100 $1000
Cost per kg to Moon $1000 $1000

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