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    Title

    Interactive Presentations - IAF SPACE PROPULSION SYMPOSIUM

    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 ten 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

    2018-10-04

    Time

    13:15

    Room

    IP Hall

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

    • Co-Chair: Dr. Mario Kobald, German Aerospace Center (DLR), Germany;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    13:15

    Aquasonic II – Hybrid Propulsion analysis for 3D-printed fuel grains

    10

    confirmed

    Mr. Alexander Scharf

    Hochschule Bremen

    Germany

    2

    13:25

    Conceptual design of a hybrid sounding rocket to reach a target altitude

    10

    confirmed

    Dr. Jeongmoo Huh

    Queen Mary University of London

    United Kingdom

    5

    13:35

    Design of a High Thrust Short Duration Solid Motor for Crew Escape System

    10

    Mr. khadar voli

    Indian Space Research Organization (ISRO)

    India

    6

    13:45

    Design and Experimental Analysis of Hybrid Rocket Engine Additively Manufactured Complex Port Geometries

    10

    confirmed

    Mr. Alec Yenawine

    University of Miami

    United States

    7

    13:55

    EFFECT OF PYROLYSIS AND OXIDATION OF N-DECANE ON THE HEAT AND MASS TRANSFER CHARACTERISTICS OF HYDROCARBON FUELED SUPERSONIC FILM COOLING

    10

    confirmed

    Ms. Jingying Zuo

    Harbin Institute of Technology

    China

    8

    14:05

    Control System of LE-9 Engine using Electric Drive Valves

    10

    confirmed

    Mr. Yusuke Funakoshi

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    9

    14:15

    High porosity open cell metal foam supported catalysts for decomposition of 98% hydrogen peroxide

    10

    withdrawn

    Dr. Pawel Surmacz

    Institute of Aviation

    Poland

    10

    14:25

    Development of a Consistent Burn Rate Determination Methodology for Ballistic Evaluation Motor

    10

    Mr. KIRAN PINUMALLA

    Vikram Sarabhai Space Centre, Thiruvananthapuram-695 022, INDIA

    India

    11

    14:35

    An overview of electric propulsion activities of Shanghai Institute of Space Propulsion

    10

    withdrawn

    Dr. Guanrong Hang

    Shanghai Institute of Space Propulsion

    China

    12

    14:45

    Laser Ablation Propulsion Launch System (LAPLaS) as a basis for New Access-to-Space Paradigm.

    10

    confirmed

    Mr. IOURI PIGULEVSKI

    Switzerland

    13

    14:55

    Effect of Prestrain on Uniaxial Tensile Behavior of HTPB Composite Propellant

    10

    confirmed

    Mr. Jiming CHENG

    Northwestern Polytechnical University

    China

    14

    15:05

    A simplified chemical reaction mechanism for two-component RP-3 kerosene surrogate fuel and its verification

    10

    confirmed

    Dr. Yingwen YAN

    Nanjing University of Aeronautics and Astronautics

    China

    15

    15:15

    Two-dimensional tomographic reconstruction in combustion flows using multiple absorption transitions

    10

    confirmed

    Dr. Junling Song

    Academy of Eqiupment

    China

    16

    15:25

    CFD design method for capacitive POGO suppressor devices

    10

    withdrawn

    Mr. Benoit CINGAL

    ArianeGroup

    France

    17

    15:35

    Experimental Investigation of Injectors Design and their Effects on 1kN Performance Hybrid Rocket Motor

    10

    confirmed

    Mr. Mohammed Bouziane

    Royal Military Academy

    Belgium

    18

    15:45

    Additive Manufacturing Technologies applied to Space Propulsion

    10

    confirmed

    Mr. David Ritz

    Sitael Spa

    United States

    19

    15:55

    Experimental Studies of the 150N HAN-based Monopropellant Attitude Control thruster

    10

    confirmed

    Mrs. Guo Manli

    Shanghai Institute of Space Propulsion

    China

    20

    16:05

    Experimental Evaluation of the effect of Swirl oxidizer injection and aluminum particle addition in N2O-paraffin wax based laboratory Hybrid Rocket Propulsion System

    10

    withdrawn

    Mr. Sachin S Kukke

    India

    21

    16:15

    Numerical study of temperature field during composite case co-curing process

    10

    confirmed

    Ms. Qun Liang

    Northwestern Polytechnical University

    China

    22

    16:25

    Design and fabrication of MEMS thrust measurement system for performance evaluation of MEMS thruster

    10

    confirmed

    Mr. Youngsuk Ryu

    Hanbat National University

    Korea, Republic of

    23

    16:35

    Energy conversion in wall catalytic steam reforming of hydrocarbon fuel at supercritical pressures

    10

    confirmed

    Prof. Silong Zhang

    Harbin Institute of Technology

    China

    24

    16:45

    Life Cycle Prediction Of A Liquid Propellant Rocket Engine Thrust Chamber Using Unified Chaboche Viscoplastic Model

    10

    confirmed

    Mr. A.K. Asraff

    Indian Space Research Organization (ISRO)

    India

    25

    16:55

    The Zurqui Engine: The First Central American and Caribbean Liquid Rocket Engine

    10

    withdrawn

    Mr. Roy Ramirez

    Purdue University

    Costa Rica

    26

    17:05

    Gelled propellant rocket motor and gas generator technology in Germany - an overview -

    10

    confirmed

    Dr. Karl Wieland Naumann

    Bayern Chemie

    Germany

    27

    17:15

    LES of HTPB/O2 and HTPB/N2O hybrid rocket engines

    10

    withdrawn

    Dr. Antonella Ingenito

    Sapienza University of Rome

    Italy

    28

    17:25

    ARCLIGHT - A low cost plug-and-play RIT electric propulsion system

    10

    confirmed

    Dr. Philipp Bauer

    ArianeGroup

    Germany

    29

    17:35

    Design, Analysis and Test of a Hybrid Rocket Engine with a Multi-port Nozzle

    10

    withdrawn

    Mr. Hamed Gamal

    SpaceForest

    Poland

    30

    17:45

    Cold Flow Simulation of Compound Swirling Oxidizer Injection for Hybrid Rocket Propulsion

    10

    withdrawn

    Mr. Shota Goto

    Kyushu Institute of Technology

    Japan

    31

    17:55

    Results of Field-Emission Cathode Operation on the H-II Transfer Vehicle

    10

    confirmed

    Dr. Yasushi Ohkawa

    JAXA

    Japan

    32

    18:05

    Convolutional neural network based combustion mode classification for condition monitoring in a supersonic combustor

    10

    confirmed

    Mr. Xiaobin Zhu

    National University of Defense Technology

    China

    33

    18:15

    Development of a 25kN Hybrid Rocket Engine for the Stratos III sounding rocket

    10

    confirmed

    Mr. Dion Anthony van Strydonck

    Delft University of Technology (TU Delft)

    The Netherlands

    34

    18:25

    Electric propulsion system based on the air-breathing radio-frequency ion thruster using the upper atmosphere gases as propellant

    10

    confirmed

    Mr. Svyatoslav Gordeev

    Research Institute of Applied Mechanics and Electrodynamics (RIAME), MAI

    Russian Federation

    35

    18:35

    Status of Orion European Service Module Propulsion Subsystem Qualification Testing

    10

    confirmed

    Mr. Benedikt Determann

    ArianeGroup

    Germany

    36

    18:45

    effect of chevron-like injector outlet on vortex-driven combustion instability

    10

    confirmed

    Mr. Guangxu Wang

    National Key LAB of Science and Technology on LRE

    China

    37

    18:55

    acoustic analysis on sub-scaled gas generator

    10

    confirmed

    Mr. Guangxu Wang

    National Key LAB of Science and Technology on LRE

    China

    38

    19:05

    Student Designed Propulsion System for a Reusable Flight Vehicle

    10

    confirmed

    Mr. Eric Perry

    University of Southern California

    United States

    39

    19:15

    Development of an Electro Thermal CubeSat Pulsed Plasma Thruster

    10

    withdrawn

    Mr. James Bultitude

    International Space University (ISU)

    United States

    40

    19:25

    Research on Failure Criterion of High Energy Solid Propellant under Complex Stress State

    10

    confirmed

    Mr. YAO Dong

    CASC

    China

    41

    19:35

    Plume Analysis of ADN Green Propellant Thruster for Satellite Attitude Control

    10

    withdrawn

    Prof. Kyun Ho Lee

    Sejong University

    Korea, Republic of

    42

    19:45

    Experimental Investigations of Plume Characteristics of the HET-40 Hall Thruster by Langmuir Probe

    10

    confirmed

    Dr. JIA LIU

    Shanghai Institute of Space Propulsion

    China

    43

    19:55

    Effect of Nozzle Geometry on Counterflow Jets for Drag Reduction of a High Speed Vehicle

    10

    confirmed

    Mr. Jaecheong Lee

    Chungnam National University

    Korea, Republic of

    44

    20:05

    3D imaging of burning aluminum particles in solid propellant using digital inline holography

    10

    confirmed

    Dr. Bingning JIN

    Northwestern Polytechnical University

    China

    45

    20:15

    LOx/LH2 engine demo platform

    10

    confirmed

    Mr. Sébastien PRIOTTO

    ArianeGroup

    France

    46

    20:25

    Transient Model of API Injector Using EcoSimPro for Expander Bleed Engine Application

    10

    withdrawn

    Mr. Robson Hahn

    DLR (German Aerospace Center)

    Germany

    47

    20:35

    Parameters analysis of non-linear combustion instability base on the pulsed trigger T-burner technique

    10

    withdrawn

    Dr. Bingning JIN

    Northwestern Polytechnical University

    China

    48

    20:45

    DEVELOPMENT AND TESTING OF AN ADDITIVE LAYERED MANUFACTURED NOZZLE FOR A COLD GAS MICRO THRUSTER

    10

    confirmed

    Mr. Abdelfattah Mostafa

    Omnidea-RTG GmbH

    Germany

    49

    20:55

    Radiographic Inspection and Analysis of Case Bonded Solid Rocket Motor Defects

    10

    confirmed

    Dr. ACHUTANANDA PARHI

    Indian Space Research Organization (ISRO)

    India

    50

    21:05

    development of the mems-based nozzle using drie of tapered hole technology for cube satellite

    10

    confirmed

    Mr. GIWON LA

    Hanbat National University

    Korea, Republic of

    51

    21:15

    A new European approach for Electric Propulsion on Small Satellites: HiperLoc-EP

    10

    withdrawn

    Dr. Jeongmoo Huh

    Queen Mary University of London

    United Kingdom

    52

    21:25

    Prediction and Validation of the Catalytic Decomposition of Hydrogen Peroxide in Dual-Catalytic Bed

    10

    confirmed

    Mr. Sangwoo Jung

    Korea Advanced Institute of Science and Technology (KAIST)

    Korea, Republic of

    53

    21:35

    A NEW SEMI-ANALYTICAL MODEL FOR PRELIMINARY ESTIMATION OF ION NUMBER DENSITY IN ELECTRIC THRUSTER PLUME

    10

    confirmed

    Mr. Andrea Binci

    Sapienza University of Rome

    Italy

    54

    21:45

    Control of Exhaust Gas Flow in Cryogenic Storage Tank Adopting Thermodynamic Venting System Technology

    10

    confirmed

    Dr. zhenjun zhou

    China Academy of Launch Vehicle Technology (CALT)

    China

    55

    21:55

    modeling and simulation of steady-state characteristics of cryogenic rocket engine

    10

    withdrawn

    Mr. Yanbo Gong

    Beijing Aerospace Propulsion Institute

    China

    56

    22:05

    Design concepts and numerical simulation on the solid propellant microthruster for cubesat

    10

    withdrawn

    Prof. Shipeng Li

    Beijing Institute of Technology, School of Aerospace Engineering

    China

    56

    22:05

    structural integrity analysis of srm grain at low temperature ignition

    10

    confirmed

    Mr. YAO Dong

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

    China