WEBVTT 99:59:59.999 --> 99:59:59.999 The problem is 99:59:59.999 --> 99:59:59.999 00:00when the capsule moves from an elliptical orbit to a parabolic orbit. There's no mathematical formula for that. 99:59:59.999 --> 99:59:59.999 00:09 Because we can calculate launch and landing but without this conversion the capsule stays in orbit, we can't bring it back home. 99:59:59.999 --> 99:59:59.999 00:18 Maybe we've been thinking about this all wrong. 99:59:59.999 --> 99:59:59.999 00:20 How's that? 99:59:59.999 --> 99:59:59.999 00:26 Maybe it's not new math at all. 99:59:59.999 --> 99:59:59.999 00:30 It could be old math. 99:59:59.999 --> 99:59:59.999 00:32 Something that looks at the problem numerically and not theoretically. Math is always dependable. 99:59:59.999 --> 99:59:59.999 00:39 For you it is. 99:59:59.999 --> 99:59:59.999 00:47 Euler's method. 99:59:59.999 --> 99:59:59.999 00:49 Euler's method? 99:59:59.999 --> 99:59:59.999 00:50 Yes. That's ancient. But it works. 99:59:59.999 --> 99:59:59.999 00:54 It works numerically. 99:59:59.999 --> 99:59:59.999 01:31 That's it. 99:59:59.999 --> 99:59:59.999 01:35 Let's type it up. 99:59:59.999 --> 99:59:59.999 01:40 Huh.