Timeline for Design of return trajectory from lunar polar orbit to Earth's atmosphere
Current License: CC BY-SA 4.0
5 events
| when toggle format | what | by | license | comment | |
|---|---|---|---|---|---|
| May 31, 2019 at 2:38 | answer | added | uhoh | timeline score: 1 | |
| May 30, 2019 at 17:07 | comment | added | Russell Borogove | According to this paper patched conics were used for the Voyager and Galileo missions as a starting point for numerical simulation. That is: solve your trajectory using patched conics, take that solution into a full N-body simulation, and make small corrections to it until it's acceptable for your purposes. | |
| May 30, 2019 at 17:02 | comment | added | Russell Borogove | related: how to best patch my conics? | |
| May 30, 2019 at 16:10 | review | First posts | |||
| May 30, 2019 at 16:21 | |||||
| May 30, 2019 at 16:08 | history | asked | Chloe | CC BY-SA 4.0 |