Ablative heat shield studies for NASA Mars/Earth return entry vehicles
Approved for public release; distribution unlimited. === A material that behaves likes a glassy ablator on the surface, has a low thermal conductivity, is structurally tough, lightweight, and is in some sense reusable, would be desirable for the protective heat shield used on Earth entry vehicles. A...
| Main Author: | |
|---|---|
| Other Authors: | |
| Published: |
Monterey, California: Naval Postgraduate School
2013
|
| Online Access: | http://hdl.handle.net/10945/34895 |