IAF Digital Library

2

session 2

Title: Propulsion System (2)
type: oral
Description: This session is dedicated to all aspects of Solid and Hybrid Propulsion.
Date: 2013-09-24
Time: 09:45
Room: 208A

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	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1		Solid rocket motors choices for Ariane 6 launcher	15'	confirmed	Mr. Didier Boury	Herakles (Safran group)	France
2		Demonstration Technology Activities for Ariane 6 PPH Solid Rocket Motors Stages	15'	confirmed	Mr. Philippe Cloutet	Herakles, Safran group	France
3		Characterization of the Ballistic Properties of the Novel ALAN-7 Solid Rocket Propellant	15'	confirmed	Mr. Hein Olthof	Delft University of Technology (TU Delft)	The Netherlands
4		experimental investigation of the pressure coupled responses of composite propellant with different ammonium perchlorate particles size	15'	confirmed	Mr. Bingning Jin	Northwestern Polytechnical University	China
5		Development of the Quasi-3D Model for the Grain Burnback Analysis of SRM's	15'	confirmed	Mr. Arnau Pons Lorente	Escola Tècnica Superior d'Enginyeries Industrial i Aeronàutica de Terrassa (ETSEIAT), Universitat Politècnica de Catalunya	China
6		Multi-objective Optimization of Hybrid Rocket Motor and Decision-making Using a Hyper-Radial Visualization Method	15'	confirmed	Mr. Xingliang Sun	Beijing University of Areonautics and Astronautics	China
7		experimental investigation on a lab-scale hybrid rocket burning N2O/paraffin-based fuel and N2O/metal-loaded HTPB	15'	confirmed	Ms. Francesca Scaramuzzino	Second University of Naples, SUN	Italy
8		Visualization of Hybrid Combustion between Paraffin and Gaseous Oxygen	15'	withdrawn	Ms. Elizabeth Jens	Stanford University	United States
9		Observation of the surface regression behavior of hybrid rocket fuel using a slab motor	15'	confirmed	Dr. Yutaka Wada	Akita University	Japan
10		Regression Rate Models versus experimental Results for Hybrid Rocket Engines based on H2O2 and HTPB/Al	15'	confirmed	Mr. Dennis Porrmann	Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR)	Germany
11		Numerical Simulation of Unsteady Non-Equilibrium Flows of Hybrid Rocket Ignition using Size-Optimized Reaction Mechanism	15'	confirmed	Mr. Shota Yamanaka	University of Tokyo	Japan
12		Aspects regarding hybrid combustion instability control	15'	confirmed	Prof. Sterian Danaila	University POLITEHNICA of Bucharest - Research Center for Aeronautics and Space	Romania