Range control during initial phases of supercircular reentries
For direct reentry from a lunar or deep space mission, considerable variation in reentry plane, reentry point, and reentry angle must be anticipated. The returning vehicle must therefore, possess the ability to control its range after reentry in order to touch down in the desired recovery area. Re...
| Main Author: | |
|---|---|
| Other Authors: | |
| Format: | Others |
| Language: | en_US |
| Published: |
Virginia Polytechnic Institute
2016
|
| Subjects: | |
| Online Access: | http://hdl.handle.net/10919/64680 |