Thermal Testing of Planetary Probe Thermal Protection System Materials in Extreme Entry Environments
Abstract
The present talk provides an overview of recent updates to NASA’s IHF and AEDC’s H3 high temperature arcjet test facilities that to enable higher heatflux (>2000 W/cm2) and high pressure (>5 atm) testing of TPS.
- Publication:
-
11th International Planetary Probe Workshop
- Pub Date:
- June 2014
- Bibcode:
- 2014LPICo1795.8062G