session 2

Title: Propulsion System (2)
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	Selection result	Mode	Presentation status	Speaker	Affiliation	Country
1	VEGA Solid Rocket Motors Qualification Status after Launcher Maiden Flight	accepted	15'	confirmed	Mr. Marco Fiorillo	AVIO S.p.A.	Italy
2	Solid Rocket Motors for Future European Launcher	accepted	15'	confirmed	Mr. Didier Boury	Herakles (Safran group)	France
3	Segmented srm pressure oscillation demonstrator	accepted	15'	confirmed	Mr. GIORGIO MASTRANGELO	Europropulsion	France
4	Strategies of the Grain Configuration Design for Large Solid Booster Motors	accepted	15'	no-show	Dr. Jeenu Raghavan	Indian Space Research Organization (ISRO)	India
5	Twin Screw Process Demonstration Technology Activities for Solid Propulsion in New Generation Launcher Applications	accepted	15'	confirmed	Dr. Sabine Saint Martin	SME - Safran	France
6	Experimental Study of Collision of Al/Al2O3 Condensed Particles at Various Velocities by an Innovative Method	accepted	15'	no-show	Mr. Shengyong Xia	College of Astronautics, Northwestern Polytechnical University	China
7	ORPHEE project synthesis for hybrid propulsion	accepted	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	accepted	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	accepted	15'	confirmed	Prof. Luciano Galfetti	Politecnico di Milano	Italy
10	"Pariffin-Based Hybrid Rocket Testing At The Butte AeroTec Facility"	accepted	15'	confirmed	Mr. David Micheletti	Universal Technical Resource Services	United States
11	Visualization of the Liquid Layer Combustion of Paraffin Fuel at Elevated Pressures	accepted	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	accepted	15'	confirmed	Mr. Masaki Adachi	The University of TOKYO, Graduate school	Japan
13	Numerical simulation based optimization of segmented grain for hybrid rocket motor	accepted	Poster	no-show	Mr. Dalin Rao	Beijing University of Aeronautics and Astronautics (BUAA)	China
14	Nitrous Oxide Safety for Hybrid Rockets	accepted	Poster	no-show	Mr. Jonah Zimmerman	Stanford University	United States
15	Numerical investigation of effect of grain configuration on Start-up transient in Solid Rocket Motors	accepted	Poster	no-show	Mr. Jayaprakash Janardhanan Nair	Indian Space Research Organization (ISRO)	India
16	Solid Rocket Motor Ballistic Simulator with Non-Homogeneous Burning Rate Distribution	accepted	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	accepted	Poster	confirmed	Mr. Junfeng Wu	Beijing University of Aeronautics and Astronautics (BUAA)	China
18	Combustion efficiency behavior of hybrid rocket with h2o2 catalytic decomposition	accepted	Poster	confirmed	Dr. Eun Sang Jung	Korea Advanced Institute of Science and Technology (KAIST)	Korea, Republic of
19	Three-dimensional numerical simulation of the flow field in hybrid rocket motor with wagon-wheel fuel grain	accepted	Poster	confirmed	Mr. Xintian Li	Beihang University	China
20	Performance characterization of the hybrid rocket motor with secondary injection	accepted	Poster	confirmed	Mr. Junhai Li	China Academy of Space Technology (CAST)	China
21	Regression Rate Measurements for Hybrid Rocket Engines based on GOX and HTPB	accepted	Poster	withdrawn	Mr. Dennis Porrmann	Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR)	Germany
22	NUMERICAL SIMULATION OF THE TRANSITION PROCESS IN A HYBRID ROCKET MOTOR	accepted	Poster	confirmed	Ms. Jia Yu	Beihang University	China
23	Roll Torque Prediction in SRM: Practical Applications	accepted	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	accepted	Poster	confirmed	Mr. Adrian Chelaru		Romania
25	Development of an experimental lab-scale set up for transient combustion investigation in hybrid rockets	accepted	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	accepted	Poster	confirmed	Mr. Yoshihide Hirata	Kyushu University	Japan
27	Paraffin-based fuels filled with lithium-based additives characterization	accepted	Poster	confirmed	Prof. Luciano Galfetti	Politecnico di Milano	Italy
28	Development of a solid rocket motor for the Stratos II rocket	accepted	Poster	withdrawn	Mr. Hein Olthof	T-Minus Engineering BV	The Netherlands

session 2

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