IAF Digital Library

5

session 5

Title: Propulsion Technology (2)
type: oral
Description: This session includes all science and technologies supporting all aspects of space propulsion. An objective is to attract papers from students and young professionals with a more technical rather than programmatic or organisational focus.
Date: 2017-09-28
Time: 09:45
Room: Hall E3

IPC members

Co-Chair: Mr. Walter Zinner, ArianeGroup, Germany;
Co-Chair: Mr. Jacques Gigou, European Space Agency (ESA), France;
Rapporteur: Mr. Zvika Zuckerman, Rafael Advanced Defense Systems Ltd., Israel;
Rapporteur: Mr. Max Calabro, The Inner Arch, France;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	09:45	KEYNOTE: The 1200kN-thrust-class LOX/Kerosene Rocket Engine for China New Generation Launch Vehicle	30'	withdrawn	Dr. Hui CHEN	Xi'an Aerospace Propulsion Institute	China
2	10:15	Modelling of Lunar Lander’s Thruster’s Exhaust Plume Impingement in Vacuum	15	no-show	Mr. Mrigank Sahai		India
3	10:30	Experimental investigation of self-excited combustion instabilities with injection coupling in a cryogenic rocket combustor	15	confirmed	Mr. Wolfgang Armbruster	German Aerospace Center (DLR)	Germany
4	10:45	Numerical Analysis of Combustion and Regenerative Cooling in LOX-Methane Rocket Engine	15	confirmed	Mr. Abhishek Sharma	Indian Space Research Organization (ISRO)	India
5	11:00	Performance evaluation of water - hot gas ejector system used in liquid rocket engines	15	confirmed	Dr. Ganesh Paramasivan	ISRO Propulsion Complex, Mahendragiri, India	India
6	11:15	Optical Diagnostics for Characterization of Hypergolic Ignition in a Paraffin-Based Hybrid Rocket	15	withdrawn	Mr. Keith Stober	Stanford University	United States
7	11:30	Modeling and experimental validation for the passive Thermodynamic Vent System (TVS) of cryogenic propellant tank	13	confirmed	Mr. JunHyuk Bae	Korea Advanced Institute of Science and Technology (KAIST)	Korea, Republic of
8	11:43	Visco-plastic cyclic stress analysis of a semi-cryogenic engine thrust chamber	15	confirmed	Mr. Krishnajith Jayamani	Indian Space Research Organization (ISRO), Liquid Propulsion Systems Centre (LPSC)	India
9	11:58	catalyst development and testing for ADN-fuel blends	15	confirmed	Dr. Robert-Jan Koopmans		Austria
10	12:13	the flow characteristics study of floating ring seal of liquid rocket engine	15	withdrawn	Mr. zhuang suguo	Xi'an Aerospace Propulsion Institute	China
11	12:28	Effects of numerical simulation models on thermal characteristics of combustion gas flow ejected from gas oxygen/kerosene rocket engine	15	confirmed	Dr. Junya Yuan	Beihang University (BUAA)	China
12	12:43	Challenges in Realizing Instrumentation and Remote control systems for Testing Cryogenic Engine and stage	15	confirmed	Mr. elayaperumal ezhilrajan	Indian Space Research Organization (ISRO)	India
13	12:58	sensitivity analysis of static parameters for the lox/kerosene rocket engine	15	confirmed	Dr. haohai xu	School of Astronautics,Northwestern Polytechnical University	China
14	13:13	Periodic atomization of impinging injectors modulated by back pressure fluctuations	15	withdrawn	Dr. Anlong Yang	Xi'an Aerospace Propulsion Institute	China