<font color="yellow">"Apollo was *steerable*????? How so? "</font><br /><br />It had and RCS that allowed the craft to be rolled. The capsule had an offest center of gravity which meant that there was more lift in one direction than another. This lift was used to steer up, down, left, right. When the craft was on target for a fully ballistic trajectory to hit the landing target, the craft was put into a slow roll to nullify direction changes due to the lift.<br /><br /><font color="yellow">"Waht was the crossrange ability? "</font><br /><br />I can't find it for Apollo using a quick search. Here's a bit from a history on the Gemini-program. It had a 50 km crossrange, with an l/d ratio of .18. Apollo had a ratio about twice that. DUnno if the relationship is linear or not thoug. Figure at least twice though, so 100km or more.<br /><br /><i>"There was only one significant event left before Conrad and Gordon wrapped up their mission. A secondary objective called for the crew to make an automatic reentry. The commanders of other Gemini flights had flown their spacecraft down from 120,000 meters, using the spacecraft's offset center of gravity to generate lift for changes in direction. This had enabled them to make corrections up to 550 kilometers downrange and 50 kilometers crossrange. Conrad, however, would not fly the spacecraft with his handcontroller in conjunction with computer directions; the spacecraft would follow these commands automatically.46<br /><br />On 15 September 1966, after 70:41 hours of flight and in the 44th revolution of Earth, the retrorockets fired. Conrad and Gordon watched the computer closely. It certainly seemed to be working right. Conrad then disengaged his handcontroller and put the system on automatic. When the first crossrange errors developed, the computer commanded bank angle changes. On several occasions, the spacecraft displayed an almost human characteristic, hesitating before accepting its orders. But the system</i>