Space/Science — HabitableZone

Space/Science » in reply to "Unfortunately all proposed CEV designs that I have seen are CM derivative." Mine aren't.

Okay, you have my attention. What's the shape?

Better yet, give me a ballistic coefficient, L/D ratio and a nose radius. I'm assuming this is for lunar return. Are you assuming fixed angle-of-attack with roll modulation? If so then your trajectory would probably be a partial skip out to keep the G loading below 9 Gs followed by atmospheric return to parachute deployment that kept the heat flux near a constant optimal value. Are you assuming an ablator heat shield? Reusable heatshields don't exist for lunar return.

Gary

Log in or register to post.

The whole thread (20 posts)