I really appreciate your sleuthing to find some real numbers.<br /><br />I've seen the 1300 figure for earth irradiance and the 1700 for in-space; I don't have the tools to measure it, so I don't really know. It's not as important as houw many watts you get out of each kg on-orbit.<br /><br />$1000/kg <i>is</i> low, but you're missing a crucial factor (which will become apparent in a moment); your 10w/kg is likewise poorly chosen for a space-based system. Deployable solar arrays of over 100w/kg already exist, and prototypes and research demonstrators are showing that 500w/kg could be achievable. So a 1200Mw solar array (man, if I goof on the decimal, help me out) masses 12,000,000kg with today's tech, and just 2,400,000kg with tomorrow's.<br /><br />Likewise, deployable waveguides and other gosamer structures are going to be used to keep the thing light. These components will probably be made to self-assemble to as high a degree as possible. It seems reasonable to me that the solar array will be the most massive component, but let's say it's just half the weight of the whole satellite.<br /><br />So we've got 24million kg to get to orbit.<br /><br />Do you really think you're going to pay even $1000/kg to loft that? The market will come up with a way to do it for alot less.<br /><br />Suppose we want to build this in a reasonable length of time: 5 years. Heck, let's make it 2000 days. That's 12,000kg per day, every day. If you showed there was a market for that, your launch costs woud drop through the floor.<br /><br />This also shows that it's worth it to work for 5 years to develop the 500w/kg solar arrays, since then the whole thing launches with just 2400kg/day. Oh, looky there, that's the load a K1 can deliver! And that's not even the optimal delivery tool. I researched around with some cutting-edge folks, and there's a way to deliver cargo to orbit for alot less (any regular on the boards knows the real reason launch costs are inflexibly high, so this thread doesn't need t