session IP

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: 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
Order	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	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	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	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	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
5	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	Effect of residual strain on structural integrity of SRM grain during ignition	10	withdrawn	Mr. Jiming CHENG	Northwestern Polytechnical University	China
7	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
8	Ring Rockets	10	no-show	Mr. Oleg Aleksandrov	Private individual www.oleg.space	United States
9	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	The P-5 Engine: A Costa Rican, Cost-effective, Low Power Liquid Rocket Engine	10	confirmed	Mr. Roy Ramirez	Purdue University	United States
11	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	plasma assisted nitrous oxide direct thermal \\decomposition and combustion for hybrid rocket	10	confirmed	Mr. Myoungjin Kim	Chosun University	Korea, Republic of
13	Optimum Design of LOX Recirculation System in KSLV-II 1st stage	10	withdrawn	Dr. Youngsuk Jung	Korea Aerospace Research Institute (KARI)	Korea, Republic of
14	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	Development and Testing of a High-Performance 3D Printed Inconel Resistojet	10	confirmed	Mr. Giulio Coral	University of Tokyo	Japan
16	Plume Simulation of HAN Thruster for Green Propellant Application	10	no-show	Prof. Kyun Ho Lee	Sejong University	Korea, Republic of
17	Innovative VRD Solution for Deep Space Missions	10	confirmed	Mr. Volodymyr Astapenko	SPACE HUB Incubator	Ukraine
18	The LH2/LOX cryogenic propulsion technology for future deep space exploration	10	withdrawn	Ms. Han JI	Beijing Union University	China
19	The cryogenic propulsion technology for future deep space exploration	10	confirmed	Ms. Han JI	Beijing Union University	China
20	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
21	The IPG6-B as a research facility to support future development of electric propulsion	10	confirmed	Mr. Jens Schmidt	Baylor University	Germany
22	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	characterization of an adaptive hall thruster	10	withdrawn	Mr. Nicholas Proulx	Royal Military College	Canada
24	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	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
26	experimental and numerical study on charging properties of cigarette granules under electrostatic field	10	no-show	Mr. bowen Yang	Harbin Institute of Technology	China
27	effect of combustion on supersonic film cooling by hydrocarbon	10	no-show	Mr. Li Xingtai		China
28	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
29	On The Effects Of Thermoacoustics on Soot Formation and Flame Instability	10	confirmed	Mr. Rahul Ravi Ravichandran	SRM University, kattankulathur,chennai,INDIA	India
30	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	combustion and propulsive characteristics of potential hybrid rocket propellant	10	no-show	Mr. Aditya Virkar	SRM University, kattankulathur,chennai,INDIA	India
32	THE PROJECTS OF THE RAPID INTERSTELLAR EXPEDITIONS.	10	no-show	Mr. Oleg Aleksandrov	Private individual www.oleg.space	United States
33	Preliminary evaluation of Engine Health Monitoring for Hall thruster	10	withdrawn	Mr. Christopher Andrea Paissoni	Politecnico di Torino	Italy
34	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	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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