Thermal Testing of Planetary Probe TPS in Extreme Entry Environments

High temperature testing of thermal protection system (TPS) materials is a critical aspect of heat-shield materials development, as it determines the suitability and performance envelope of the materials. The present talk provides an overview of recent updates to NASAs IHF and AEDCs H3 high temperature arcjet test facilities that to enable higher heat flux (5000-8000 Wcm2) and high pressure (5-14 atm) testing of TPS. Some recent thermal tests of fully dense carbon phenolic will be discussed in this paper. These new facility upgrades will help improve the TRL level of novel TPS materials and will help qualifycertify heritage TPS material candidates for future missions that are expected to encounter extreme entry conditions, such as entry into Venus or Saturn.