Good analogy, I like that. I am a big skeptic on analysis by analogy, but I like this one.<br /><br />I think I figgered out how to claim this is on-topic. What are those rocket engineers at XCOR up to, anyway? Well I don't know, so I'll distract them by talking about their fellow rocketeers while you go peek under their tent. <br /><br />Besides, I went to the latest Armadillo thread and it was all about Rutan lately. <img src="/images/icons/laugh.gif" /><br /><br />I'm just saying I see Armadillo as being in competition with a steam catapault; they both move the near shore out a bit. In Carmack's case, he's trying to move it all the way out to the deep channel where there's little resistance to speeding up. You'll never steam catapult out to the deep channel of space. The whole idea of trying to outfox the rocket equation, that's good stuff, but steam catapult? <br /><br />By going up to 101.6 kilometers, you have invested 1.400 km/sec in potential energy. You have also incurred gravity and drag losses. Well, you weren't accelerating to orbit, so drag losses will be not that high, I'll SWAG a number like, oh, say, um, 0.10 km/s and then we have to figure gravity losses.<br /><br />dVgrav = g,eff * t,b * sin(phi)<br />g,eff = local gravity on the way up<br />t,b = time of burn in seconds<br />phi = flight angle<br />sin(phi) = 1.00 for straight up flight<br />g = GM / (R)^2<br />Rb = Re + altitude<br />Earth: Re = 6371 km<br />Earth's GM = 398600.44 km^3 / s^2<br />altitude = 101.6 km<br />Rb = 6371 + 101.6 = 6473 km<br />g, end of flight = 3.986E5 / 6473^2 = .009514 km/s^2<br />g,eff = ( 9.807 + 9.513 ) / 2 = 9.6605 m / s^2<br /><br />y = ½ a * t^2<br />t = sqrt( (2 * y) / a)<br />y = 101600 m<br />a = 1.43 "gees" = 14.11 m / s^2<br />t = 120 seconds<br /><br />So a two minute flight would have<br />9.6605 * 120 = 1159 m / s <br />1.16 km/s in gravity losses<br /><br />All together, he's going to need<br />1.400 + 1.16 + 0.1 <br />= 2.66 km/s deltaV performance from his rocket powered elevator to spac <div class="Discussion_UserSignature"> </div>