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  • session IP

    Title

    Interactive Presentations - IAF SPACE PROPULSION SYMPOSIUM

    type

    interactive

    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: Dr. Vanessa Vial, SAFRAN, 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

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    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

    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

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

    10

    confirmed

    Dr. Qiaofeng Xie

    Tsinghua University

    China

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

    10

    confirmed

    Dr. cheng cheng

    Shanghai Insitute of Space Propulsion

    China

    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

    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

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

    10

    confirmed

    Mr. Roy Ramirez

    Purdue University

    United States

    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

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

    10

    confirmed

    Mr. Myoungjin Kim

    Chosun University

    Korea, Republic of

    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

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

    10

    confirmed

    Mr. Giulio Coral

    University of Tokyo

    Japan

    Innovative VRD Solution for Deep Space Missions

    10

    confirmed

    Mr. Volodymyr Astapenko

    SPACE HUB Incubator

    Ukraine

    The cryogenic propulsion technology for future deep space exploration

    10

    confirmed

    Ms. Han JI

    Beijing Union University

    China

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

    10

    confirmed

    Mr. Jens Schmidt

    Baylor University

    Germany

    Overview of Research on Nuclear Thermal Rocket Nozzles at OSU

    10

    confirmed

    Mr. Nick Salamon

    The Ohio State University College of Engineering

    United States

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

    10

    confirmed

    Ms. Qun Liang

    Northwestern Polytechnical University

    China

    On The Effects Of Thermoacoustics on Soot Formation and Flame Instability

    10

    confirmed

    Mr. Rahul Ravi Ravichandran

    SRM University, kattankulathur,chennai,INDIA

    India

    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

    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