rootbrowseIAC-17D2session 33. Upper Stages, Space Transfer, Entry and Landing SystemsPapers1. Suitability of reusability and in-situ propellant production for a Lunar transportation system2. Development of the European Service Module Propulsion Subsystem for the Multi-Purpose Crew Vehicle3. Characterization of Direct Metal Laser Sintered Impinging Injectors: Like-Doublet, Unlike Triplet, Like Quadlet, Unlike Pentad4. Docking mechanism for the STRONG mission: design, mathematical modeling, and experimental testing5. The adaptive algorithm of separation program for a nanosatellites cluster from space platform executed uncontrolled motion6. deep machine learning in vision based hazard detection for autonomous planetary landings: advancements and ground validation7. Development of Supersonic Descent Vehicle Reconfiguration Rapid Analysis Methodology for Application to Human-class Mars Entry, Descent, and Landing8. Flexible Landing System for Exploration of Rocky Celestial Bodies9. Mission Scenarios Utilizing LOTUS: Lander/Orbiter Trans-Upper Stage10. Conceptual Design Synthesis Methodology Application for an Orbital Reentry Generic Wing-Body Configuration11. Uncertainty-based Multidisciplinary Design Optimization for Launch Vehicle12. Shapeable Hypersonic Waverider for Mars Entry