IAF Digital Library

2

session 2

Title: Propulsion System (2)
type: oral
Description: This session is dedicated to all aspects of Solid and Hybrid Propulsion.
Date: 2018-10-02
Time: 09:45
Room: ZARM 5

IPC members

Co-Chair: Mr. Stéphane Henry, France;
Co-Chair: Dr. Toru Shimada, Institute of Space and Astronautical Science (ISAS), Japan Aerospace Exploration Agency, Japan;
Rapporteur: Dr. Yen-Sen Chen, American Institute of Aeronautics and Astronautics (AIAA), United States;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	09:45	KEYNOTE: Recent developments in solid propulsion	30	confirmed	Mr. Jean-Francois Guery	ArianeGroup	France
2	10:15	Flight Results of Solid Propulsion System for Epsilon Launch Vehicle from the Third Flight	15	confirmed	Dr. Koki Kitagawa	Japan Aerospace Exploration Agency (JAXA), ISAS	Japan
3	10:30	Research on thermochemical reaction mechanism and model of EPDM insulator under slag deposition condition	15	confirmed	Dr. Yiwen Guan	Northwestern Polytechnical University，NPU	China
4	10:45	Assessment of the Flight Experiments of a Multifunction Hybrid Sounding Rocket	15	confirmed	Dr. Yen-Sen Chen	American Institute of Aeronautics and Astronautics (AIAA)	Taiwan, China
5	11:00	Technology Development for a Potential Hybrid Mars Ascent Vehicle	15	confirmed	Dr. Ashley Karp	Jet Propulsion Laboratory - California Institute of Technology	United States
6	11:15	Effect of Pressure Loss Devices on the Performance of Hybrid Rocket Systems	15	confirmed	Prof.Dr. Arif Karabeyoglu	Koc University	United States
7	11:30	A Study on Throttling, Anti-O/F Shift Operation and LOX Vaporization for Hybrid Rocket Engine with Multi-Section Swirl Injection Method	15	confirmed	Prof. Shigeru Aso	Kyushu University	Japan
8	11:45	Characterization of Regression Rate and Combustion Process in a High-Pressure 2D Hybrid Rocket Engine with Optical Access	15	confirmed	Mr. Georg Poppe	German Aerospace Center (DLR)	Germany
9	12:00	The preliminary study of severity level of structural discontinuities in paraffin grain of hybrid propellant rocket	15	confirmed	Dr. Artem Andrianov	University of Brasilia	Brazil
10	12:15	Experimental Investigation of the Feed System Instabilities in Hybrid Rocket Motors	15	confirmed	Prof. Artur Bertoldi	University of Brasilia	Brazil
11	12:30	Validation Against Experimental Data of Numerical Prediction of Characteristics of Combustion Instability in Hybrid Rocket Motors	15	confirmed	Mr. Goutham Karthikeyan	Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency	Japan