Well, to be honest, much is gleaned from reading the Boeing, Lockheed/Martin and Northrop/Grumman trade studies final documents and taking educated guesses, extrapolated up from Apollo designs.<br /><br />That post was started by me to see if all the smart and in-the-know people on this forum could correct me on my estimates, and discuss what the real masses and propulsion choices might be for these spacecraft and boosters.<br /><br />For example, I've postulated that the lunar lander might have a launch weight of 30 tons; nearly twice that of the Apollo LM. I've expected someone to say; you're wrong -- the Lunar Lander would weigh 25, 35 or even 40 tons. But NO ONE has responded to my post to kick off this potentially fascinating nuts-and-bolts discussion.<br /><br />I'm disappointed to say the least! <div class="Discussion_UserSignature"> <p> </p><p>One Percent of Federal Funding For Space: America <strong><em><u>CAN</u></em></strong> Afford it!! LEO is a <strong><em>Prison</em></strong> -- It's time for a <em><strong>JAILBREAK</strong></em>!!</p> </div>