In Situ Small Spacecraft Missions Utilizing Heatshield for Extreme Entry Environments Technology
Advanced Rigid Ablative Thermal Protection Systems
Mars 2020 Thermal Protection Systems Sizing and Development
In Situ Small Spacecraft Missions Utilizing Heatshield for Extreme Entry Environments Technology
Heat Pipes for Space Applications Part 1 - Axially Grooved Heat Pipes
Thermal Margins for Flight Electronics Review and Assessment
Woven Thermal Protection System: Heatshield for Extreme Entry Environment Technology (HEEET)
Robust and Mass Efficient Thermal Protection Systems for Future Venus Missions
TPS and Entry Systems Technologies for Future Mars and Titan Exploration
Comparing Particle Flow Regimes in the L2K Arcjet with Martian Entry Conditions
2007-01-1525 Experimental Study of Automotive Cooling Fan Aerodynamics
A comparative analysis of loop heat pipe based thermal architectures for spacecraft thermal control
Laboratory Testing of Vehicle and Industrial Heat Exchangers for Thermal Cycle Durability
3D Printing Heat Shields: An Overview of the AMTPS Project
Entry Systems Modeling and Ground Testing: Enabling Flight Performance and Risk Reduction