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    Title

    Interactive Presentations

    Description

    This session offers a unique opportunity to deliver your key messages in an interactive presentation on any of the subjects of Space Propulsion addressed in the classic Sessions. The presentation will be displayed on a digital screen in a dedicated location and available for view by all Congress attendees for the entire Congress week. In addition, one afternoon is dedicated exclusively for the attendees to view the Interactive Presentations, and the author will be assigned a specific eight minute slot to personally present the topic and interact with the attendees present. The Interactive Presentation may take advantage of all electronic display capabilities, such as: PowerPoint charts, embedded hot links, pictures, audio and video clips etc. An award will also be presented to the author of the best Interactive Presentation in the C Category at a special ceremony. An Abstract that follows the standard format must be submitted by the deadline for standard IAC abstracts.

    Date

    2017-09-28

    Time

    12:45

    Room

    Hall J&K2

    IPC members
    • Co-Chair: Dr. Elizabeth Jens, Jet Propulsion Laboratory - California Institute of Technology, United States;

    • Co-Chair: Ms. Elizabeth Driscoll, GomSpace Aps, United States;

    • Co-Chair: Dr. Jerrol Littles, Aerojet Rocketdyne, United States;

    • Co-Chair: Mr. Christophe Bonhomme, Centre National d'Etudes Spatiales (CNES), France;

    • Co-Chair: Dr. Yen-Sen Chen, American Institute of Aeronautics and Astronautics (AIAA), United States;

    papers

    Order

    Presentation status

    Mode

    Paper title

    Speaker

    Affiliation

    Country

    1

    confirmed

    Spacecraft-plasma interactions of a cubesat equipped with miniaturized feep thrusters

    Mr. Amenosis Lopez

    TU Braunschweig

    Germany

    2

    confirmed

    Advanced Propulsion Control System(APCS) Model using Intelligent Techniques

    Mr. elayaperumal ezhilrajan

    Indian Space Research Organization (ISRO)

    India

    3

    confirmed

    Transient Responses of Turbulent Heat Transfer of N-Decane at Supercritical Pressure and Temperature below 800 K

    Dr. Bo Ruan

    School of Aeronautics and Astronautics, Dalian University of Technology

    China

    4

    withdrawn

    design, manufacture and testing of a 20 cm electron cyclotron resonance gridded ion thruster and neutraliser using additive manufacturing

    Mr. Jacob Verlander

    University of Southampton

    United Kingdom

    5

    confirmed

    wavelet packet analysis of time-frequency characteristic of the LOX/Kerosene rocket engine due to heavy impact

    Dr. Feiping Du

    Xi'an Aerospace Propulsion Institute

    China

    6

    confirmed

    Application of Particle-In-Cell Simulation Techniques in the Analysis and Optimisation of Magnetic Nozzle Geometries

    Mr. Alexander Ryan

    University of New South Wales

    Australia

    7

    confirmed

    Multi-objective Design Optimization of the Cusped Field Thruster for Micro-Satellite Platforms

    Mr. Thomas Logan Fahey

    RMIT University (Royal Melbourne Institute of Technology)

    Australia

    8

    confirmed

    Study of Effect of Neutral Flow and Electron Transport in Wall Less Hall Thruster Concept

    Mr. Rohan M Ganapathy

    Bellatrix Aerospace Private Limited

    India

    9

    confirmed

    Control of Miniaturized Electrospray Ion Thrusters for CubeSat Designs

    Mr. Samuel Laprise

    Ecole Polytechnique de Montreal

    Canada

    10

    withdrawn

    Coilgun Acceleration Model Containing Interactions Between Multiple Coils

    Ms. Connie Liu

    Georgia Institute of Technology, School of Aerospace Engineering

    United States

    11

    confirmed

    Overview of Electric Propulsion Developments at TU Dresden for Micro and Small-Satellites

    Prof. Martin Tajmar

    TU Dresden

    Germany

    12

    withdrawn

    investigation of selective laser melting (slm) for production of microwave ion thruster accelerator grids

    Mr. David Hoffman

    University of Southampton

    United Kingdom

    13

    withdrawn

    Evaluation of Quasi-Steady Operation of MPD Thruster using Electric Double-Layer Capacitors

    Mr. Shunichiro Ide

    The University of TOKYO, Graduate school

    Japan

    14

    confirmed

    Closed-loop Thrust Control for Micropropulsion Systems

    Mr. Stefano Silvestrini

    Delft University of Technology (TU Delft)

    The Netherlands

    15

    confirmed

    choi-williams ditribution analysis for fault detection of the liquid propellant rocket engine

    Dr. Feiping Du

    Xi'an Aerospace Propulsion Institute

    China

    16

    confirmed

    Numerical Simulation of Flow Characteristics in Methane Transverse Jet

    Mr. zengkai shi

    China

    17

    withdrawn

    Two Dimensional Axisymmetric Navier-Stokes Analysis of Hybrid Rocket Intrinsic Instability

    Mr. Goutham Karthikeyan

    Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency

    Japan

    18

    confirmed

    Study of Ignition Transient in 2m Diameter Segmented SRM

    Dr. Jian-ru Wang

    The 41st Institute of the Fourth Academy, China Aerospace Science and Technology Corporation (CASC)

    China

    19

    confirmed

    An additively-manufactured CNG/GOX aerospike rocket engine: Test results, performance and analysis

    Mr. Nicholas Mason-Smith

    Monash University

    Australia

    20

    confirmed

    Study on auto-ignited hybrid rocket based on n2o oxidizer using catalytic ignition system

    Mr. Jincheol Kim

    Chosun University

    Korea, Republic of

    21

    confirmed

    Early Studies and Fire Tests of a Green Liquid Apogee Engine Based on Decomposition of 98% Hydrogen Peroxide

    Dr. Pawel Surmacz

    Institute of Aviation

    Poland

    22

    withdrawn

    Applications for 3D printing in the Design of Hall Effect Thrusters

    Mr. Ethan Hopping

    University of Alabama in Huntsville

    United States

    23

    confirmed

    Effect of Prestrain on Dynamic Mechanical Properties of HTPB propellant

    Prof. Jinxian Li

    Science and Technology on Combustion, Internal Flow and Thermal-structure Laboratory,Northwestern Polytechnical University

    China

    24

    withdrawn

    numerical investigation on detonation process of pulse detonation engine with hypergolic propellants

    Dr. Hongbo HU

    Xian Aerospace Propulsion Institute

    China

    25

    confirmed

    investigation of catalytic re-ignition process in hydrogen peroxide hybrid rocket motors

    Dr. Sheng Zhao

    China Academy of Launch Vehicle Technology (CALT)

    China

    26

    confirmed

    numerical simulation of catalytic decomposition and combustion process in an hydroxylammonium nitrate (han)-based monopropellant thruster

    Ms. Xiqiao Yu

    Shanghai Insitute of Space Propulsion

    China

    27

    confirmed

    Assessment of combustion instability mechanisms based on an energy balance analysis

    Mr. Arnau Pons Lorente

    Purdue University

    United States

    28

    confirmed

    Investigation on the Near-nozzle Field Flow of Liquid Jet in a Supersonic Crossflow

    Mr. Liyin Wu

    China Aerodynamics Research and Development Center (CARDC) 

    China

    29

    withdrawn

    A Theoretical Study on Throttle Ranges of O/F Controllable Hybrid Rocket Propulsion Systems

    Dr. Kohei Ozawa

    Kyushu Institute of Technology

    Japan

    30

    confirmed

    Numerical simulation of the start process of a han-based mono-propellant rocket thruster

    Prof.Dr. Dechuan Sun

    School of Aeronautics and Astronautics, Dalian University of Technology

    China

    31

    confirmed

    Systematic performance analysis of cubesat propulsion systems using the high performance satellite dynamics simulator HPS

    Dr. Benny Rievers

    ZARM University of Bremen

    Germany

    32

    confirmed

    Development of 2,500 N class hydrogen peroxide/polyethylene hybrid rocket for lab-scale sounding rocket application

    Mr. Yongtae Yun

    Korea Advanced Institute of Science and Technology (KAIST)

    Korea, Republic of

    33

    confirmed

    Numerical Simulation of Influence of Injector Parameters on Combustion in LOX/Methane Engine

    Prof. Ping Jin

    School of Astronautics, Beihang University

    China

    34

    confirmed

    Material Compatibility of Six Metal Alloys with HAN based Green Monopropellant Fuel Blend

    Mr. Rohan M Ganapathy

    Bellatrix Aerospace Private Limited

    India

    35

    confirmed

    particle damping characteristics of low and medium frequency oscillation in solid rocket motor

    Ms. Shaojuan Wei

    Northwestern Polytechnical University,NPU

    China

    36

    withdrawn

    Feasibility of FDM Ablative Ceramic Materials for Low-Cost Propulsive Systems

    Mr. Adam Bower

    University of Alabama in Huntsville

    United States

    37

    withdrawn

    Optimization of catalytic bed geometry for 98% hydrogen peroxide monopropellant thruster

    Mr. Przemyslaw Paszkiewicz

    Warsaw University of Technology (WUT)

    Poland

    38

    confirmed

    Shallow Water Tests of Seconary Injection Thrust Vector Control of Aerospike Nozzles

    Mr. Christian Bach

    Dresden University of Technology (DUT) / Technische Universität Dresden

    Germany

    39

    withdrawn

    Numerical and experimental study of supersonic film cooling with cracking hydrocarbon fuel as coolant

    Mr. Kunlin Cheng

    Harbin Institute of Technology

    China

    40

    confirmed

    Design and Experimental Characterization of a Hydrogen Peroxide-Ethanol based Combustor for Space Propulsion

    Mr. Disip Chaturvedi

    Indian Institute of Technology, Bombay

    India

    42

    confirmed

    Primary In-Space Experimental results of the HEP-100MF Electrical Propulsion System

    Prof.Dr. Yan Shen

    Beijing Insitude of Control Engineering

    China

    43

    withdrawn

    Reusable TSTO Conceptual Vehicle Designs using the TRRE Engine

    Dr. Peiran Su

    Science and Technology on Scramjet Laboratory, Beijing Power Machinery Research Institute

    China

    44

    withdrawn

    Turbine reheater: a new paradigm for hypersonic flight propulsion

    Prof. Sterian Danaila

    University POLITEHNICA of Bucharest - Research Center for Aeronautics and Space

    Romania

    45

    withdrawn

    LES of Streamwise Vortex on Supersonic Mixing employing Hypermixer

    Mr. Sheng Guo

    Science and Technology on Scramjet Laboratory,Beijing Power Machinery Research Inst

    China

    46

    Experimental and Computational Studies of Supersonic Combustion Characteristics of HyperMixer in Mach 8 Flight Condition

    Dr. Yang Fujiang

    Science and Technology on Scramjet Laboratory, The 31st Research Institute of CASIC

    China

    47

    withdrawn

    Preliminary studies on physical definition and discrimination of rocket-ejector mode of RBCC Engine

    Dr. Feiteng Luo

    Science and Technology on Scramjet Laboratory, Beijing Power Machinery Research Institute

    China

    48

    The preliminary study of severity level of structural discontinuities in paraffin grain of hybrid propellant rocket

    Dr. Artem Andrianov

    University of Brasilia

    Brazil

    49

    Analysis of cavitation characteristics of pumps used in liquid rocket engines by using multihole orifice plate

    Mr. RAHUL KUMAR CHAURASIA

    Indian Space Research Organization (ISRO)

    India

    50

    confirmed

    On the Electrical Propulsion of a Solar Sail

    Ms. Elena Ancona

    Telespazio VEGA Deutschland GmbH

    Germany

    51

    confirmed

    Physical grounds and control optimization of ultralow-orbit spacecraft with electric ramjet

    Dr. Olga Yanova

    TsAGI

    Russian Federation