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: 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
Paper title	Mode	Presentation status	Speaker	Affiliation	Country
Aquasonic II – Hybrid Propulsion analysis for 3D-printed fuel grains	10	confirmed	Mr. Alexander Scharf	Hochschule Bremen	Germany
Conceptual design of a hybrid sounding rocket to reach a target altitude	10	confirmed	Dr. Jeongmoo Huh	Queen Mary University of London	United Kingdom
Design of a High Thrust Short Duration Solid Motor for Crew Escape System	10		Mr. khadar voli	Indian Space Research Organization (ISRO)	India
Design and Experimental Analysis of Hybrid Rocket Engine Additively Manufactured Complex Port Geometries	10	confirmed	Mr. Alec Yenawine	University of Miami	United States
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
Control System of LE-9 Engine using Electric Drive Valves	10	confirmed	Mr. Yusuke Funakoshi	Japan Aerospace Exploration Agency (JAXA)	Japan
High porosity open cell metal foam supported catalysts for decomposition of 98% hydrogen peroxide	10	withdrawn	Dr. Pawel Surmacz	Institute of Aviation	Poland
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
An overview of electric propulsion activities of Shanghai Institute of Space Propulsion	10	withdrawn	Dr. Guanrong Hang	Shanghai Institute of Space Propulsion	China
Laser Ablation Propulsion Launch System (LAPLaS) as a basis for New Access-to-Space Paradigm.	10	confirmed	Mr. IOURI PIGULEVSKI		Switzerland
Effect of Prestrain on Uniaxial Tensile Behavior of HTPB Composite Propellant	10	confirmed	Mr. Jiming CHENG	Northwestern Polytechnical University	China
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
Two-dimensional tomographic reconstruction in combustion flows using multiple absorption transitions	10	confirmed	Dr. Junling Song	Academy of Eqiupment	China
CFD design method for capacitive POGO suppressor devices	10	withdrawn	Mr. Benoit CINGAL	ArianeGroup	France
Experimental Investigation of Injectors Design and their Effects on 1kN Performance Hybrid Rocket Motor	10	confirmed	Mr. Mohammed Bouziane	Royal Military Academy	Belgium
Additive Manufacturing Technologies applied to Space Propulsion	10	confirmed	Mr. David Ritz	Sitael Spa	United States
Experimental Studies of the 150N HAN-based Monopropellant Attitude Control thruster	10	confirmed	Mrs. Guo Manli	Shanghai Institute of Space Propulsion	China
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
Numerical study of temperature field during composite case co-curing process	10	confirmed	Ms. Qun Liang	Northwestern Polytechnical University	China
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
Energy conversion in wall catalytic steam reforming of hydrocarbon fuel at supercritical pressures	10	confirmed	Prof. Silong Zhang	Harbin Institute of Technology	China
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
The Zurqui Engine: The First Central American and Caribbean Liquid Rocket Engine	10	withdrawn	Mr. Roy Ramirez	Purdue University	Costa Rica
Gelled propellant rocket motor and gas generator technology in Germany - an overview -	10	confirmed	Dr. Karl Wieland Naumann	Bayern Chemie	Germany
LES of HTPB/O2 and HTPB/N2O hybrid rocket engines	10	withdrawn	Dr. Antonella Ingenito	Sapienza University of Rome	Italy
ARCLIGHT - A low cost plug-and-play RIT electric propulsion system	10	confirmed	Dr. Philipp Bauer	ArianeGroup	Germany
Design, Analysis and Test of a Hybrid Rocket Engine with a Multi-port Nozzle	10	withdrawn	Mr. Hamed Gamal	SpaceForest	Poland
Cold Flow Simulation of Compound Swirling Oxidizer Injection for Hybrid Rocket Propulsion	10	withdrawn	Mr. Shota Goto	Kyushu Institute of Technology	Japan
Results of Field-Emission Cathode Operation on the H-II Transfer Vehicle	10	confirmed	Dr. Yasushi Ohkawa	JAXA	Japan
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
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
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
Status of Orion European Service Module Propulsion Subsystem Qualification Testing	10	confirmed	Mr. Benedikt Determann	ArianeGroup	Germany
effect of chevron-like injector outlet on vortex-driven combustion instability	10	confirmed	Mr. Zhanyi Liu	National Key LAB of Science and Technology on LRE	China
acoustic analysis on sub-scaled gas generator	10	confirmed	Dr. Chen Hongyu		China
Student Designed Propulsion System for a Reusable Flight Vehicle	10	confirmed	Mr. Eric Perry	University of Southern California	United States
Development of an Electro Thermal CubeSat Pulsed Plasma Thruster	10	withdrawn	Mr. James Bultitude	International Space University (ISU)	United States
Research on Failure Criterion of High Energy Solid Propellant under Complex Stress State	10	confirmed	Mr. YAO Dong	CASC	China
Plume Analysis of ADN Green Propellant Thruster for Satellite Attitude Control	10	withdrawn	Prof. Kyun Ho Lee	Sejong University	Korea, Republic of
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
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
3D imaging of burning aluminum particles in solid propellant using digital inline holography	10	confirmed	Dr. Bingning JIN	Northwestern Polytechnical University	China
LOx/LH2 engine demo platform	10	confirmed	Mr. Sébastien PRIOTTO	ArianeGroup	France
Transient Model of API Injector Using EcoSimPro for Expander Bleed Engine Application	10	withdrawn	Mr. Robson Hahn	DLR (German Aerospace Center)	Germany
Parameters analysis of non-linear combustion instability base on the pulsed trigger T-burner technique	10	withdrawn	Dr. Bingning JIN	Northwestern Polytechnical University	China
DEVELOPMENT AND TESTING OF AN ADDITIVE LAYERED MANUFACTURED NOZZLE FOR A COLD GAS MICRO THRUSTER	10	confirmed	Mr. Abdelfattah Mostafa	Omnidea-RTG GmbH	Germany
Radiographic Inspection and Analysis of Case Bonded Solid Rocket Motor Defects	10	confirmed	Dr. ACHUTANANDA PARHI	Indian Space Research Organization (ISRO)	India
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
A new European approach for Electric Propulsion on Small Satellites: HiperLoc-EP	10	withdrawn	Dr. Enric Grustan-Gutiérrez	Queen Mary University of London	United Kingdom
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
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
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
modeling and simulation of steady-state characteristics of cryogenic rocket engine	10	withdrawn	Mr. Yanbo Gong	Beijing Aerospace Propulsion Institute	China
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
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

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