An analysis of the static and dynamic characteristics of a decoupled landing entry vehicle
A theoretical analysis of the static and dynamic characteristics of an entry vehicle utilizing the decoupled landing concept has been conducted. A hypersonic arbitrary-body aerodynamic computer program was used to determine the aerodynamics of the basic body. Three theories were used and compared wi...
| Main Author: | |
|---|---|
| Other Authors: | |
| Format: | Others |
| Language: | en_US |
| Published: |
Virginia Polytechnic Institute
2016
|
| Subjects: | |
| Online Access: | http://hdl.handle.net/10919/64581 |