rootbrowseIAC-05D2session 55. Future Space Transportation Systems TechnologiesPapers1. Next Generation Launcher: CNES approach and associated Demonstration Logic2. Numerical Analysis of Reverse Jet Effect on the aerodynamic characteristics of SSTO configuration with an Aerospike Nozzle in Landing Phase3. Improvement of Aerodynamic Performances for Reusable Launch Vehicles Using the Lateral Blowing4. Investigation of Cryogenic Solid Propulsion Application for Large Solid Rocket Boosters5. Development of Cryogenic Composite Tank Lined with Polymer Film6. Development of X-43A Mach 10 Leading Edges7. Final Report of HSFD Phase II Transport Flight Data Evaluation by CFD Simulations8. Advanced Development Projects for Constellation from the Next Generation Launch Technology Program Elements9. Analysis of shockwave interactions for a Generic Space Plane Configuration at hypersonic speeds and estimation of heat flux generation on the structure10. A New Thermal Protection System by Opposing Jet for Reusable Launch Vehicle