IAF Digital Library

3

session 3

Title: Propulsion Technology (1)
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: 2014-10-01
Time: 09:45
Room: 714B

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		An overview of experimental activities and results addressing the development of LOX/LCH4 rocket engine technology in the Italian HYPROB program	15'	confirmed	Dr. Vito Salvatore	CIRA Italian Aerospace Research Center, Capua	Italy
2		Status and Future Perspectives of the CMC Rocket Thrust Chamber Development at DLR	15'	confirmed	Mr. Markus Ortelt	Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR)	Germany
3		European Cold Gas Micro Propulsion System reached TRL-9 on board GAIA S/C. Discussion on in flight performance and system flexibly and capabilities, for being implemented in other missions requiring ultra-fine satellite positioning and att	15'	confirmed	Mr. Aldo Polli	Selex ES S.p.A	Italy
4		Aerojet Rocketdyne Propulsion for Next Generation GEO ComSat Platforms	15'	confirmed	Ms. Olwen Morgan	Aerojet Rocketdyne	United States
5		Feasibility Analysis and Testing Results of Cold Gas Propulsion System	15'	confirmed	Mr. Surmit Bhui	University of Petroleum and Energy Studies	India
6		Investigations on the effect of variations in characteristic length(L*) and contraction ratio of the combustion chamber on the performance of a liquid hypergolic bipropellant thruster	15'	confirmed	Dr. NARAYANAN V	Liquid Propulsion System centre	India
7		Propulsion demonstrators in ESA FLPP 3 serving the competitiveness of European launchers	15'	confirmed	Mr. Jean-Noel CARUANA	European Space Agency (ESA)	France
8		Developing and testing new composite catalytic bed for decomposition of 98% HTP	15'	confirmed	Dr. Grzegorz Rarata	Warsaw Institute of Aviation	Poland
9		A scheme study for minimizing weight of pressurization system on KSLV-II upper stage	15'	confirmed	Mr. Youngsuk Jung	Korea Aerospace Research Institute (KARI)	Korea, Republic of
10		An Experimental Study of LOX/Methane Subscale Injector	15'	confirmed	Mr. Yuan Tian	Beijing Aerospace Propulsion Institute	China
12		apogee hydrogen peroxide-ethanol rocket propulsion. ecological compatibility, safety and new power opportunities	15'	confirmed	Mr. Yulian Protsan	The Laboratory of Advanced Jet Propulsion	Ukraine
14		Experimental and numerical study of flame structure and combustion dynamics in a shear coaxial injector with GH2/GO2	15'	confirmed	Dr. Yue HAN	China Eastern Airlines Corporation Limited	China