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		KEYNOTE: Additive Layer Manufacturing will change rocket liquid propulsion	30'	confirmed	Mr. Marc Vales	Airbus Safran Launchers	France
2		overview of le-9 engine development for h3 launch vehicle	15'	confirmed	Mr. Nobuki Negoro	Mitsubishi Heavy Industries, Ltd.	Japan
3		VULCAIN 2.1®, the European reference for Ariane 6 Lower stage cryogenic engine	15'	confirmed	Mr. Sabin Patrick		France
4		LOX/METHANE reusable rocket propulsion at reach with large scale demonstrators tested	15'	confirmed	Mr. Yoan Boué	Airbus Safran Launchers	France
5		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		Challenges in restart of pressure fed liquid upper stage	15'	confirmed	Dr. Deepak Kumar Agarwal	LPSC, ISRO	India
7		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		Vinci® Propulsion System: Transition from Ariane 5 ME to Ariane 6	15'	confirmed	Mr. Patrick Danous	Snecma	France
9		Development of an up-rated version of earth storable pump fed liquid engine for ISRO launch vehicles.	15'	withdrawn	Mr. Aneesh Rajan	LPSC, ISRO	India
10		static characteristic analysis of 180kn lox/kerosene upper stage engine	'15	confirmed	Dr. Yuanqi Li	Xian Aerospace Propulsion Institute	China
11		Development status of CE20 cryogenic engine for GSLV LVM3 vehicle	'15	no-show	Dr. Vanniyaperumal Narayanan	Indian Space Research Organization (ISRO)	India
12		Multidiscipline approach to the design and modernization of high power Liquid Propellant Engines for their reuse	15'	withdrawn	Mr. Vladimir Tkach	JSC NPO Energomash	Russian Federation
13		effect of fuel injection schemes in a vortex combustion chamber	'15	no-show	Mr. Vikash Kumar	Liquid Propulsion System centre	India
14		The design and test of 250N thruster with HAN-based propellant	'15	confirmed	Mr. xin Qiu	Shanghai Institute of Space Propulsion	China
15		Multidisciplinary design optimization of a spacecraft bi-propellant propulsion system using a computationally improved framework	15'	withdrawn	Mr. H.R. Fazeley	K. N. Toosi University of Technology	Iran