IAF Digital Library

2

session 2

Title: Propulsion Systems II
Description: This session is dedicated to all aspects of Solid and Hybrid Propulsion.
Date: 2010-09-28
Time: 10:15
Room: Club A

IPC members

Chairman: Mr. Jean-François Guery, Safran SME, France;
Chairman: Dr. I-Shih Chang, The Aerospace Corporation, United States;
Rapporteur: Mr. Jacques Gigou, European Space Agency (ESA), France;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1		S200 SOLID BOOSTER DEVELOPMENT	15	withdrawn	Mr. Abraham P J	Indian Space Research Organization (ISRO)	India
2		Performance Prediction for the first Static Test of a Large Solid Booster Motor	15	confirmed	Mr. Jayaprakash Janardhanan Nair	Indian Space Research Organization (ISRO)	India
3		Zefiro 9A – VEGA Third Stage Solid Rocket Motor - Development Activities and Lessons Learnt	15	confirmed	Mr. Stefano Bianchi	European Space Agency (ESA)	Italy
4		Thrust Anomalies at Ignition Transient of Solid Propellant Rockets	15	confirmed	Prof. Bernardo Favini	Sapienza Università di Roma	Italy
5		SRB Acoustic and Plume Analysis of Ares I-X Flight Test On The Pad B Fixed Service Structure	15	confirmed	Mr. Roger X. Lenard	LPS	United States
6		development of advanced computer science for solid-rocket-motor internal ballistics: acssib	15	confirmed	Dr. Toru Shimada	Japan Aerospace Exploration Agency (JAXA)	Japan
7		Overview of Large Solid Rocket Motor Options for Future European Launcher	15	confirmed	Mr. Didier Boury	Herakles (Safran group)	France
8		Paraffin-Based/LOX Hybrid Rocket Development and Testing	15		Mr. David A. Micheletti	MSE Technology Applications, Inc.	United States
9		Development of 2500 N Class CAMUI Type Hybrid Rocket for Winged Flight Experiments	15	confirmed	Prof. Harunori Nagata	Hokkaido University	Japan
10		A NEW CHALLENGE FOR IMPROVEMENT OF RECESSION RATE OF HIGH DENSITY POLYETHYLENE FUEL AND PARAFFIN FUEL OF HYBRID ROCKET WITH MULTI-SECTION SWIRL INJECTION	15	confirmed	Prof. Shigeru Aso	Kyushu University	Japan
11		Experimental Evaluation of a High Test Peroxide Catalyst Chamber for a Hybrid Rocket Engine	15	withdrawn	Mr. Daniel Lancelle	Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR)	Germany
12		Design and Development of Paraffin/N2O Hybrid Propulsion System with Catalytic Igniter	15	confirmed	Prof. Taegyu Kim	Chosun University	Korea, Republic of
–		Improvement of Combustion Mechanism of Hybrid Rocket of High Density Polyethylene Fuel with Multi-Section Swirl Injection		confirmed	Prof. Shigeru Aso	Kyushu University	Japan