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
Effect of residual strain on structural integrity of SRM grain during ignition	10	withdrawn	Mr. Jiming CHENG	Northwestern Polytechnical University	China
Ejector Developing of Vacuum Ignition Test System for Upper-stage LH2-LOX Rocket Engines	10	no-show	Mr. Fanchao Kong	Beijing Institute of Aerospace Testing Technology	China
Ring Rockets	10	no-show	Mr. Oleg Aleksandrov	Private individual www.oleg.space	United States
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
Optimum Design of LOX Recirculation System in KSLV-II 1st stage	10	withdrawn	Dr. Youngsuk Jung	Korea Aerospace Research Institute (KARI)	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
Plume Simulation of HAN Thruster for Green Propellant Application	10	no-show	Prof. Kyun Ho Lee	Sejong University	Korea, Republic of
Innovative VRD Solution for Deep Space Missions	10	confirmed	Mr. Volodymyr Astapenko	SPACE HUB Incubator	Ukraine
The LH2/LOX cryogenic propulsion technology for future deep space exploration	10	withdrawn	Ms. Han JI	Beijing Union University	China
The cryogenic propulsion technology for future deep space exploration	10	confirmed	Ms. Han JI	Beijing Union University	China
Determination of Composite Solid Propellant Relaxation Modulus Master Curves From Dynamic Mechanical Analysis	10	withdrawn	Mr. Wagner Kim Amaral Silva	Avibras Indústria Aeroespacial S.A.	Brazil
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
characterization of an adaptive hall thruster	10	withdrawn	Mr. Nicholas Proulx	Royal Military College	Canada
Influence rule and global sensitivity analysis of parameters during cure process of SRM composite case	10	confirmed	Ms. Qun Liang	Northwestern Polytechnical University	China
numerical simulation study on oxidation coking of hydrocarbon fuel in the presence of electrostatic field	10	no-show	Ms. Dan Jin	Harbin Institute of Technology	China
experimental and numerical study on charging properties of cigarette granules under electrostatic field	10	no-show	Mr. bowen Yang	Harbin Institute of Technology	China
effect of combustion on supersonic film cooling by hydrocarbon	10	no-show	Mr. Li Xingtai		China
the effect of the regenerative cooling process on the supersonic combustion inside a strut-based supersonic combustor	10	no-show	Ms. Huimin Tian	Harbin Institute of Technology	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
combustion and propulsive characteristics of potential hybrid rocket propellant	10	no-show	Mr. Aditya Virkar	SRM University, kattankulathur,chennai,INDIA	India
THE PROJECTS OF THE RAPID INTERSTELLAR EXPEDITIONS.	10	no-show	Mr. Oleg Aleksandrov	Private individual www.oleg.space	United States
Preliminary evaluation of Engine Health Monitoring for Hall thruster	10	withdrawn	Mr. Christopher Andrea Paissoni	Politecnico di Torino	Italy
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
Electric propulsion’s rational application range on the small spacecrafts	10	no-show	Mr. Alexey Sidorov	Dnipropetrovsk National University named after Oles Gonchar	Ukraine

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