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  • session 3

    Title

    Upper Stages, Space Transfer, Entry and Landing Systems

    type

    oral

    Description

    Discussion of existing, planned or new advanced concepts for cargo and human orbital transfer. Includes current and near term transfer, entry and landing systems, sub-systems and technologies for accommodating crew and cargo transfer in space.

    Date

    2017-09-27

    Time

    09:45

    Room

    Hall O

    IPC members
    • Co-Chair: Dr. Oliver Kunz, Beyond Gravity, Switzerland;

    • Co-Chair: Dr. Chiara Manfletti, ESA, France;

    • Co-Chair: Mr. Brian Smith, Raytheon Canada Limited, Canada;

    • Rapporteur: Mr. Oleg Ventskovskiy, Ukraine;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Suitability of reusability and in-situ propellant production for a Lunar transportation system

    15

    confirmed

    Mr. Etienne Dumont

    Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR)

    Germany

    2

    Development of the European Service Module Propulsion Subsystem for the Multi-Purpose Crew Vehicle

    15

    confirmed

    Dr. George Schmidt

    NASA Glenn Research Center

    United States

    3

    Characterization of Direct Metal Laser Sintered Impinging Injectors: Like-Doublet, Unlike Triplet, Like Quadlet, Unlike Pentad

    15

    withdrawn

    Mr. Deepak Atyam

    Purdue University

    United States

    4

    Docking mechanism for the STRONG mission: design, mathematical modeling, and experimental testing

    15

    confirmed

    Dr. Tharek Mohtar

    Politecnico di Torino

    Italy

    5

    The adaptive algorithm of separation program for a nanosatellites cluster from space platform executed uncontrolled motion

    15

    confirmed

    Mr. Denis Avariaskin

    Samara National Research University (Samara University)

    Russian Federation

    6

    deep machine learning in vision based hazard detection for autonomous planetary landings: advancements and ground validation

    15

    withdrawn

    Mr. Marco Ciarambino

    Politecnico di Milano

    Italy

    7

    Development of Supersonic Descent Vehicle Reconfiguration Rapid Analysis Methodology for Application to Human-class Mars Entry, Descent, and Landing

    15

    withdrawn

    Mr. David Blette

    Georgia Institute of Technology

    United States

    8

    Flexible Landing System for Exploration of Rocky Celestial Bodies

    15

    confirmed

    Ms. Sonali Sinha Roy

    SRM University, India

    India

    9

    Mission Scenarios Utilizing LOTUS: Lander/Orbiter Trans-Upper Stage

    15

    confirmed

    Mr. Chrishma Singh-Derewa

    National Aeronautics and Space Administration (NASA), Jet Propulsion Laboratory

    United States

    10

    Conceptual Design Synthesis Methodology Application for an Orbital Reentry Generic Wing-Body Configuration

    15

    withdrawn

    Mr. Loveneesh Rana

    University of Texas at Arlington

    United States

    11

    Uncertainty-based Multidisciplinary Design Optimization for Launch Vehicle

    15

    withdrawn

    Prof. Xiaohui Wang

    Beihang University

    China

    12

    Shapeable Hypersonic Waverider for Mars Entry

    15

    withdrawn

    Mr. Jesse Maxwell

    Naval Research Laboratory

    United States