rootbrowseIAC-17D2session IPIP. Interactive PresentationsPapers1. Effect of high energy materials on performance of solid rocket motor for space missions2. terminal sliding mode control of payload re-entry using momentum exchange tether system3. The German Contribution to the Development of Ariane 64. a new three-stage-to-orbit concept utilizing rbcc propulsion technology5. Fully Reusable Two Stage to Orbit Conceptual Vehicle Design6. Comprehensive methodology for technology roadmaps generation and update for the European hypersonic and re-entry space transportation scenario7. The Critical Technologies and Applications on Advanced Upper Stage Vehicles8. The General Discussion on Thermal Technologies in Advanced Space Transfer Vehicles9. An Investigation on the staging aerodynamics of a Two-Stage-To-Orbital Vehicle Powered by RBCC Engine10. The Orbital Tether Concept for Efficient Space Access11. Parameter Optimization of Lunar Space Elevator Transportation System Based on Comprehensive Evaluation Method12. Flight Trajectory Analysis on Advanced Morphing Space Transportation System for Wider Cross Range and Down Range with Trimmed Flight13. Massdriver Capabilities of the Bodies of the Solarsystem14. The Design of TSTO Air-Breathing Launch Vehicle Trajectory15. Research on a new concept first stage of TSTO launch vehicle configuration16. Multiconditional load variable area nose (MCL-VAN)17. Technical Capabilities of Chinese Launch Vehicles18. Breaking New Grounds and Records: New Methodologies and practical applications in the convergence of aerospike motors and oceanic launch vehicles19. Demise Observation Capsule: Progress update20. sending a deep space probe for interstellar exploration21. Launch platform and Meteorology for COBO project22. Italian Contribution to the ESA Ministerial Conference 2016: next generation of the European VEGA launcher for new green and reusable space missions23. orbital transfer performance and mission applicability analysis for bare electrodynamic tethered spacecraft