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: 2015-10-13
Time: 09:45
Room: Ballroom B (Crowne Plaza Hotel, -1 floor)

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;
Rapporteur: Mr. M. Badrinayarana Murthy, Indian Space Research Organization (ISRO), India;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1		Advanced Biological Treatment for Solid Propulsion - LICORNE	15'	confirmed	Mr. Guillaume Dupouy	Herakles (Safran group)	France
2		A scaled-down static test method for solid rocket motors.	15'	confirmed	Ms. Olga Motsyk	Delft University of Technology (TU Delft)	The Netherlands
3		improvement on thrust profile flexibility by oxidizer-to-fuel ratio feedback control in hybrid rocket	15'	confirmed	Mr. Tomoaki Usuki	Institute of Space and Astronautical Science (ISAS), Japan Aerospace Exploration Agency	Japan
4		HEAT AND MASS TRANSFER ANALYSIS FOR PARAFFIN / NITROUS OXIDE BURNING RATE IN HYBRID PROPULSION	15'	confirmed	Mrs. Shani Ben-Basat	TECHNION - Israel Institute of Technology	Israel
5		Performance Calculations and Burning Tests on Altering-intensity Swirling Oxidizer Flow Type Hybrid Rocket Engines	15'	confirmed	Mr. Kohei Ozawa	Japan Aerospace Exploration Agency (JAXA), ISAS	Japan
6		PRELIMINARY DESIGN OF HYBRID GAS GENERATOR IN STAGED HYBRID ROCKET ENGINE	15'	confirmed	Prof. Changjin Lee	Konkuk University	Korea, Republic of
7		Integrated approach for hybrid rocket technology development and analysis of possible applications	15'	confirmed	Dr. Francesco Barato	University of Padova - DII/CISAS	Italy
8		Combustion Instability in SARA Hybrid Rocket Motor	15'	confirmed	Prof. Artur Bertoldi	University of Brasilia	Brazil
9		Design of a hybrid paraffin-based technology demonstrator	15'	confirmed	Dr. Marco Di Clemente	CIRA Italian Aerospace Research Centre	Italy
10		Benefits of a Hybrid Propulsion System Using In Situ Produced Oxidizer for a Mars Ascent Vehicle	15'	withdrawn	Dr. Ashley Karp	Jet Propulsion Laboratory - California Institute of Technology	United States
11		Combustion Instability Simulation and Analysis of a Solid Rocket Motor Testing Device based on LES Method	15'	confirmed	Mr. Linqing Zhang	The 41st Institute of the Sixth Academy of Aerospace Science & Industry Corp	China
12		estimation of flight specific impulse for solid propellant rocket motors	15'	withdrawn	Mr. Chamarthi Sainadh	ISRO	India