session 2

Title: Propulsion System (2)
type: oral
Description: This session is dedicated to all aspects of Solid and Hybrid Propulsion.
Date: 2012-10-02
Time: 10:15
Room: TS14 (Sala Capri, Palacongressi)

IPC members

Chairman: Mr. Stéphane Henry, France;
Chairman: Dr. I-Shih Chang, The Aerospace Corporation, United States;
Rapporteur: Dr. Toru Shimada, Institute of Space and Astronautical Science (ISAS), Japan Aerospace Exploration Agency, Japan;

papers
Order	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	VEGA Solid Rocket Motors Qualification Status after Launcher Maiden Flight	15'	confirmed	Mr. Marco Fiorillo	AVIO S.p.A.	Italy
2	Solid Rocket Motors for Future European Launcher	15'	confirmed	Mr. Didier Boury	Herakles (Safran group)	France
3	Segmented srm pressure oscillation demonstrator	15'	confirmed	Mr. GIORGIO MASTRANGELO	Europropulsion	France
5	Twin Screw Process Demonstration Technology Activities for Solid Propulsion in New Generation Launcher Applications	15'	confirmed	Dr. Sabine Saint Martin	SME - Safran	France
7	ORPHEE project synthesis for hybrid propulsion	15'	confirmed	Mr. Philippe GAUTIER	Herakles (Safran group)	France
8	Program AHRES and its contribution to assess features and current limitations of hybrid rocket propulsion	15'	confirmed	Dr. Ognjan Bozic	Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR)	Germany
9	An Italian network to improve hybrid rockets performance: the strategy, the program, the results	15'	confirmed	Prof. Luciano Galfetti	Politecnico di Milano	Italy
10	"Pariffin-Based Hybrid Rocket Testing At The Butte AeroTec Facility"	15'	confirmed	Mr. David Micheletti	Universal Technical Resource Services	United States
11	Visualization of the Liquid Layer Combustion of Paraffin Fuel at Elevated Pressures	15'	confirmed	Dr. Ashley Karp	Jet Propulsion Laboratory - California Institute of Technology	United States
12	Numerical investigation of liquified fuel characteristics in hybrid rocket engine	15'	confirmed	Mr. Masaki Adachi	The University of TOKYO, Graduate school	Japan
16	Solid Rocket Motor Ballistic Simulator with Non-Homogeneous Burning Rate Distribution	Poster	confirmed	Mr. Roberto Bertacin	Alma Mater Studiorum - University of Bologna	Italy
17	Investigation of fuel regression rate in a lab-scale n2o/htpb hybrid rocket motor	Poster	confirmed	Mr. Junfeng Wu	Beijing University of Aeronautics and Astronautics (BUAA)	China
18	Combustion efficiency behavior of hybrid rocket with h2o2 catalytic decomposition	Poster	confirmed	Dr. Eun Sang Jung	Korea Advanced Institute of Science and Technology (KAIST)	Republic of Korea
19	Three-dimensional numerical simulation of the flow field in hybrid rocket motor with wagon-wheel fuel grain	Poster	confirmed	Mr. Xintian Li	Beihang University	China
20	Performance characterization of the hybrid rocket motor with secondary injection	Poster	confirmed	Mr. Junhai Li	China Academy of Space Technology (CAST)	China
22	NUMERICAL SIMULATION OF THE TRANSITION PROCESS IN A HYBRID ROCKET MOTOR	Poster	confirmed	Ms. Jia Yu	Beihang University	China
23	Roll Torque Prediction in SRM: Practical Applications	Poster	confirmed	Prof. Fulvio Stella	Universita' di Roma 'La Sapienza'	Italy
24	A Computational Model for Stability and Sensitivity Analysis of a Classic Type Hybrid Rocket Motor	Poster	confirmed	Mr. Adrian Chelaru		Romania
25	Development of an experimental lab-scale set up for transient combustion investigation in hybrid rockets	Poster	confirmed	Dr. Laura Merotto	Politecnico di Milano	Italy
26	Performance advancement of hybrid rocket engine through higher regression rate and combustion efficiency with multi-section swirl injection method	Poster	confirmed	Mr. Yoshihide Hirata	Kyushu University	Japan
27	Paraffin-based fuels filled with lithium-based additives characterization	Poster	confirmed	Prof. Luciano Galfetti	Politecnico di Milano	Italy

session 2

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