IAF Digital Library

1

session 1

Title: Propulsion System (1)
type: oral
Description: This session is dedicated to all aspects of Liquid Rocket Engines.
Date: 2016-09-26
Time: 15:15
Room: Zapopan

IPC members

Co-Chair: Mr. Christophe Bonhomme, Centre National d'Etudes Spatiales (CNES), France;
Co-Chair: Mr. Patrick Danous, ArianeGroup, France;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	15:15	KEYNOTE: Additive Layer Manufacturing will change rocket liquid propulsion	30'	confirmed	Mr. Marc Vales	Airbus Safran Launchers	France
2	15:45	overview of le-9 engine development for h3 launch vehicle	15'	confirmed	Mr. Nobuki Negoro	Mitsubishi Heavy Industries, Ltd.	Japan
3	16:00	VULCAIN 2.1®, the European reference for Ariane 6 Lower stage cryogenic engine	15'	confirmed	Mr. Sabin Patrick		France
4	16:15	LOX/METHANE reusable rocket propulsion at reach with large scale demonstrators tested	15'	confirmed	Mr. Yoan Boué	Airbus Safran Launchers	France
5	16:30	Effect of bearing supporting stiffness on critical speed and dynamic stability of turbo-pump rotor system in LOX/Kerosene rocket engine	15'	confirmed	Dr. Feiping Du	Xi'an Aerospace Propulsion Institute	China
6	16:45	Challenges in restart of pressure fed liquid upper stage	15'	confirmed	Dr. Deepak Kumar Agarwal	LPSC, ISRO	India
7	17:00	Leveraging Additive Manufacturing for Affordable Commercial Launch Applications Enabled by the Aerojet Rocketdyne Ultra-Low-Cost Bantam Engine Family	15'	confirmed	Dr. Jerrol Littles	Aerojet Rocketdyne	United States
8	17:15	Vinci® Propulsion System: Transition from Ariane 5 ME to Ariane 6	15'	confirmed	Mr. Patrick Danous	Snecma	France
10	17:30	static characteristic analysis of 180kn lox/kerosene upper stage engine	'15	confirmed	Dr. Yuanqi Li	Xian Aerospace Propulsion Institute	China
14	17:30	The design and test of 250N thruster with HAN-based propellant	'15	confirmed	Mr. xin Qiu	Shanghai Institute of Space Propulsion	China