> <i><font color="yellow">More pie in the sky BS from a company that is trying to lure investors.</font>/i><br /><br />It is certainly that, but there is some belief that the plan could work within an order of magnitude (e.g., perhaps $20B). Here are some of the differences that I can gleam from the plan which could reduce the proposed cost:<br /><br /><font color="yellow">First,</font>this plan does not include completing, using, and servicing ISS. That is probably $30-40B right away from NASA.<br /><br /><font color="yellow">Second,</font>don't build the HLV. Instead use mission profiles that take advantage of existing MLVs. In general, each mission would involve much smaller amount of mass. Avoiding the ISS and HLV saves a lot of money.<br /><br /><font color="yellow">Third,</font>don't return directly to Earth, enter LEO first. This is similar to the t/Space plan. The LEO to Earth surface vehicle doesn't need to be over-engineered to support Beyond LEO reentry velocities. Once again, this also plays into the lack of need for an HLV.<br /><br /><font color="yellow">Fourth,</font>deliver small amounts of mass to the Lunar surface for each sortie. Did you see the "Lawn chair to the Moon" vehicles? Pretty neat, and what a ride it would be. Smaller mass means less need for HLV development. The NASA ESAS LSAM can carry 2.2 metric tons of equipment to the Lunar surface (~10 times the amount the Apollo lander could) and in a cargo-only version it can deliver 21 tons to the Lunar surface!<br /><br /><font color="yellow">Fifth,</font>optimize for the Moon. The SpaceDev plan is optimized on getting small amounts of mass to the Moon quickly. The ESAS architecture is driven by a Mars capability -- for which the HLV would play a critical role.<br /><br /><font color="yellow">Sixth,</font>increase crew risk. For example, when landing on the Moon the NASA ESAS way, you have both the LSAM pro</i>