Comparative Study of Structural Efficiencies of Typical Thermal Protection Concepts

[1]  Raphael T. Haftka,et al.  Thermal Force and Moment Determination of an Integrated Thermal Protection System , 2010 .

[2]  D. Glass Ceramic Matrix Composite (CMC) Thermal Protection Systems (TPS) and Hot Structures for Hypersonic Vehicles , 2008 .

[3]  Shuyuan Zhao,et al.  Thermo-structural optimization of integrated thermal protection panels with one-layer and two-layer corrugated cores based on simulated annealing algorithm , 2015 .

[4]  Raphael T. Haftka,et al.  (Student Paper) Analysis and Design of Corrugated-Core Sandwich Panels for Thermal Protection Systems of Space Vehicles , 2006 .

[5]  Kathryn E. Wurster,et al.  Development of Advanced Metallic-Thermal-Protection System Prototype Hardware , 2004 .

[6]  Steven Walker,et al.  The DARPA/AF Falcon Program: The Hypersonic Technology Vehicle #2 (HTV-2) Flight Demonstration Phase , 2008 .

[7]  Gauthier Picard,et al.  Dynamic Design Space Partitioning for Optimization of an Integrated Thermal Protection System , 2013 .

[8]  Songhe Meng,et al.  Structure Redesign of the Integrated Thermal Protection System and Fuzzy Performance Evaluation , 2016 .

[9]  Zheng Ye,et al.  Analysis of Reusable Integrated Thermal Protection Panel Elements with Various Insulating Core Options , 2014 .

[10]  Carl C. Poteet,et al.  Preliminary Thermal-Mechanical Sizing of a Metallic Thermal Protection System , 2004 .

[11]  Y. Prel,et al.  CMC thermal protection system for future reusable launch vehicles: Generic shingle technological maturation and tests , 2006 .

[12]  Raphael T. Haftka,et al.  Comparison of Materials for an Integrated Thermal Protection System for Spacecraft Reentry , 2009 .