IAF Digital Library

3

session 3

Title: Propulsion Technology (1)
type: oral
Description: This session included all science and technologies supporting all aspects of space propulsion. The emphasis in this session is plased in particular components for propulsion.
Date: 2016-09-28
Time: 09:45
Room: Zapopan

IPC members

Co-Chair: Mr. Didier Boury, ArianeGroup SAS, France;
Co-Chair: Dr. Angelo Cervone, Delft University of Technology (TU Delft), The Netherlands;
Rapporteur: Mr. John Harlow, Aerojet Rocketdyne, United Kingdom;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1		New Achievements in the HYPROB-BREAD LOX/LCH4 Demonstrator Development	15'	no-show	Dr. Vito Salvatore	CIRA Italian Aerospace Research Center, Capua	Italy
2		LOX/Methane Thrust Chamber Demonstrator- from Subscale to Full scale Testing	15'	confirmed	Mr. Roland Blasi	Airbus Safran Launchers	Germany
3		Spray and Combustion Characteristics of LOX/GH2 Coaxial Injectors at Supercritical Pressures	15'	no-show	Dr. Zhaobo Ding	Beijing Aerospace Propulsion Institute	China
4		ETID Sandwich Nozzle Demonstrator for Upper Stage Engines	15'	confirmed	Mr. Martin Velander	GKN Aerospace Engine Systems	Sweden
5		Additive Manufacturing and its applicability on rockets engines	15'	confirmed	Mr. Martin Velander	GKN Aerospace Engine Systems	Sweden
6		Fluidic control of transition in dual bell launcher nozzle	15'	confirmed	Mr. Vladeta Zmijanovic	ICARE-CNRS	France
7		growth of spacecraft propulsion systems in isro	15'	no-show	Mr. Banavara Krishnamurthy Venkataramu	LPSC, ISRO	India
8		Development of High Performance Liquid Apogee Motor for Geostationary Spacecraft	15'	confirmed	Dr. Deepak Kumar Agarwal	LPSC, ISRO	India
9		Extending Lifetime of Rocket Engine Combustion Chamber	15'	withdrawn	Dr. Toshiya Kimura	Japan Aerospace Exploration Agency (JAXA)	Japan
10		Investigation of Dynamics Characteristics of the Hot Gas Bellows of the LOX/Kerosene Rocket Engine	15'	withdrawn	Dr. Yuanqi Li	Xian Aerospace Propulsion Institute	China
11		numerical simulation of combustion stability of coaxial swirl injector	15'	withdrawn	Dr. Yuanqi Li	Xian Aerospace Propulsion Institute	China
12		CFD analysis of Semicryo LOX booster turbopump.	15'	confirmed	Mr. Deepak K. Agarwal	Indian Space Research Organization (ISRO)	India
13		Numerical Simulation of LRE and HRE Reacting Flowfields	15'	withdrawn	Dr. Giuliano Ranuzzi	CIRA Italian Aerospace Research Center, Capua	Italy
14		study of flow characteristics for liquid film in the impinging stream vortex chamber by cfd and experiment	15'	no-show	Mr. Jingqiu Pei	Science and Technology on Combustion, Internal Flow and Thermal-structure Laboratory, Northwestern Polytechnical University	China