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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

    2019-10-24

    Time

    13:15

    Room

    IP Area

    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

    transient simulation of the ignition over-pressure phenomenon in the altitude test of the staged-combustion-cycle rocket engine

    10

    confirmed

    Dr. Hongyue Wang

    Beijing institute of aerospace testing technology

    China

    2

    13:25

    Parametric Performance Evaluation of Liquid Injection Thrust Vector Control in Hybrid Rockets

    10

    confirmed

    Mr. Eunkwang Lee

    Korea Advanced Institute of Science and Technology (KAIST)

    Korea, Republic of

    3

    13:35

    Analysis of operating diagram for kerosene / oxygen-enriched air rotating detonation combustors under lean fuel condition

    10

    confirmed

    Dr. Qiaofeng Xie

    Tsinghua University

    China

    4

    13:45

    project ice rabbit: integrated liquid oxygen/liquid methane propulsion system for future planet exploration vehicle

    10

    Dr. cheng cheng

    Shanghai Insitute of Space Propulsion

    China

    5

    13:55

    Preliminary Design of High Speed Test Facility for Counterflow jet Experiments Reducing Heat and Drag

    10

    confirmed

    Mr. Yuseok Lee

    Chungnam National University

    Korea, Republic of

    6

    14:05

    Effect of residual strain on structural integrity of SRM grain during ignition

    10

    confirmed

    Mr. Jiming CHENG

    Northwestern Polytechnical University

    China

    7

    14:15

    Ejector Developing of Vacuum Ignition Test System for Upper-stage LH2-LOX Rocket Engines

    10

    confirmed

    Mr. Fanchao Kong

    Beijing institute of aerospace testing technology

    China

    8

    14:25

    Ring Rockets

    10

    confirmed

    Mr. Oleg Aleksandrov

    Private individual www.oleg.space

    United States

    9

    14:35

    Development of Adaptable Electrodeless Plasma Propulsion Systems Using Evolutionary Topology Optimisation and Particle in Cell Simulation

    10

    confirmed

    Mr. Alexander Ryan

    The University of Sydney

    Australia

    10

    14:45

    The P-5 Engine: A Costa Rican, Cost-effective, Low Power Liquid Rocket Engine

    10

    confirmed

    Mr. Roy Ramirez

    Purdue University

    United States

    11

    14:55

    Experimental Investigation on Drag Reduction by Plasma Counterflow Jets in Mach 7 Shock Tunnel

    10

    confirmed

    Mr. Jaecheong Lee

    Chungnam National University

    Korea, Republic of

    12

    15:05

    plasma assisted nitrous oxide direct thermal \\decomposition and combustion for hybrid rocket

    10

    confirmed

    Mr. Myoungjin Kim

    Chosun University

    Korea, Republic of

    13

    15:15

    Optimum Design of LOX Recirculation System in KSLV-II 1st stage

    10

    Dr. Youngsuk Jung

    Korea Aerospace Research Institute (KARI)

    Korea, Republic of

    14

    15:25

    development and validation of high-performance hypergolic hybrid rocket fuel ignitor with hydrogen peroxide

    10

    confirmed

    Mr. Junyeong Jeong

    Korea Advanced Institute of Science and Technology (KAIST)

    Korea, Republic of

    15

    15:35

    Development and Testing of a High-Performance 3D Printed Inconel Resistojet

    10

    confirmed

    Mr. Giulio Coral

    University of Tokyo

    Japan

    16

    15:45

    Plume Simulation of HAN Thruster for Green Propellant Application

    10

    confirmed

    Mr. Jung Won Kuk

    Sejong University

    Korea, Republic of

    17

    15:55

    Innovative VRD Solution for Deep Space Missions

    10

    confirmed

    Mr. Volodymyr Astapenko

    SPACE HUB Incubator

    Ukraine

    18

    16:05

    The LH2/LOX cryogenic propulsion technology for future deep space exploration

    10

    Ms. Han JI

    Beijing Union University

    China

    19

    16:15

    The cryogenic propulsion technology for future deep space exploration

    10

    Ms. Han JI

    Beijing Union University

    China

    20

    16:25

    Determination of Composite Solid Propellant Relaxation Modulus Master Curves From Dynamic Mechanical Analysis

    10

    confirmed

    Mr. Wagner Kim Amaral Silva

    Avibras Indústria Aeroespacial S.A.

    Brazil

    21

    16:35

    The IPG6-B as a research facility to support future development of electric propulsion

    10

    confirmed

    Mr. Jens Schmidt

    Baylor University

    Germany

    22

    16:45

    Overview of Research on Nuclear Thermal Rocket Nozzles at OSU

    10

    confirmed

    Mr. Nick Salamon

    The Ohio State University College of Engineering

    United States

    23

    16:55

    characterization of an adaptive hall thruster

    10

    confirmed

    Mr. Nicholas Proulx

    Royal Military College

    Canada

    24

    17:05

    Influence rule and global sensitivity analysis of parameters during cure process of SRM composite case

    10

    confirmed

    Ms. Qun Liang

    Northwestern Polytechnical University

    China

    25

    17:15

    numerical simulation study on oxidation coking of hydrocarbon fuel in the presence of electrostatic field

    10

    Ms. Dan Jin

    Harbin Institute of Technology

    China

    26

    17:25

    experimental and numerical study on charging properties of cigarette granules under electrostatic field

    10

    Mr. bowen Yang

    Harbin Institute of Technology

    China

    27

    17:35

    effect of combustion on supersonic film cooling by hydrocarbon

    10

    Mr. Li Xingtai

    China

    28

    17:45

    the effect of the regenerative cooling process on the supersonic combustion inside a strut-based supersonic combustor

    10

    Ms. Huimin Tian

    Harbin Institute of Technology

    China

    29

    17:55

    On The Effects Of Thermoacoustics on Soot Formation and Flame Instability

    10

    confirmed

    Mr. Rahul Ravi Ravichandran

    SRM University, kattankulathur,chennai,INDIA

    India

    30

    18:05

    Study of Dual-Catalytic Bed Scale-Up Parameters for High Test Hydrogen Peroxide Thrusters

    10

    confirmed

    Mr. Sangwoo Jung

    Korea Advanced Institute of Science and Technology (KAIST)

    Korea, Republic of

    31

    18:15

    combustion and propulsive characteristics of potential hybrid rocket propellant

    10

    confirmed

    Mr. Aditya Virkar

    SRM University, kattankulathur,chennai,INDIA

    India

    32

    18:25

    THE PROJECTS OF THE RAPID INTERSTELLAR EXPEDITIONS.

    10

    confirmed

    Mr. Oleg Aleksandrov

    Private individual www.oleg.space

    United States

    33

    18:35

    Preliminary evaluation of Engine Health Monitoring for Hall thruster

    10

    confirmed

    Mr. Christopher Andrea Paissoni

    Politecnico di Torino

    Italy

    34

    18:45

    The Effect of fuel length on the regression rate in swirling-oxidizer-flow-type hybrid rocket using a liquefying fuel

    10

    confirmed

    Mr. Yo Kawabata

    Chiba Institute of Technology

    Japan

    35

    18:55

    Electric propulsion’s rational application range on the small spacecrafts

    10

    confirmed

    Mr. Alexey Sidorov

    Dnipropetrovsk National University named after Oles Gonchar

    Ukraine