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: 2016-09-27
Time: 09:45
Room: Zapopan

IPC members

Co-Chair: Mr. Stéphane Henry, France;
Co-Chair: 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		KEYNOTE:Green Solid propellants for civilian launchers	30'	confirmed	Mr. Max Calabro	The Inner Arch	France
2		Development and qualification of S200 solid rocket booster for GSLV Mk-III	15'	confirmed	Mr. Arun Krishnan	Indian Space Research Organization (ISRO)	India
3		design and development of flex nozzle for large solid booster	15'	confirmed	Mr. V MAHESH	Indian Space Research Organization (ISRO)	India
4		Thrust Oscillations in Static Tests of Large Segmented Solid Booster of ISRO	15'	no-show	Mr. KIRAN PINUMALLA	Vikram Sarabhai Space Centre, Thiruvananthapuram-695 022, INDIA	India
5		Enhanced Epsilon Launch Vehicle and Future Plan	15'	confirmed	Mr. Hirotaka Uehara	IHI Aerospace Co, Ltd.	Japan
6		development of solid propulsion system for enhanced epsilon launch vehicle and M-35 static firing test	15'	confirmed	Dr. Koki Kitagawa	Japan Aerospace Exploration Agency (JAXA), ISAS	Japan
7		Performance Evaluation of Composite Propellant Slurry Mixing by Peristaltic Continuous Mixer	15'	confirmed	Mr. Akihiro Iwasaki	The Graduate Universty for Advanced Studies (SOKENDAI)	Japan
8		modeling distributed combustion in srm	15'	no-show	Prof. Domenico Simone	University of Brasilia	Brazil
9		Errosive burning modelling on solid rocket motors. Application to development of SRM 120.	15'	confirmed	Mr. Florin Mingireanu	Romanian Space Agency (ROSA)	Romania
10		Secondary Combustion in Staged Hybrid Rocket Engine	15'	confirmed	Mr. Dongeun Lee	Konkuk University	Korea, Republic of
11		Development of Module-Type Hybrid Rocket Engine with Multi-Section Swirl Injection Method for Flight Experiments	15'	confirmed	Prof. Shigeru Aso	Kyushu University	Japan
12		Verification of the Throttling Characteristics of Axial-injection End-burning Type Hybrid Rockets	15'	confirmed	Mr. Yuji Saito	Hokkaido University	Japan
13		Flame Emission Spectroscopy in a Paraffin-Based Hybrid Rocket	15'	confirmed	Mr. Keith Stober	Stanford University	United States
14		A test bench for the characterization of solid rocket engines: Design, construction and validation	15'	withdrawn	Dr. Javier M. Antelis	TECNOLOGICO DE MONTERREY	Mexico