session 2

Title: Propulsion System (2)
Description: This session is dedicated to all aspects of Solid and Hybrid Propulsion.
Date: 2014-09-30
Time: 09:45
Room: 714B

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	Selection result	Mode	Presentation status	Speaker	Affiliation	Country
1		A6 SRM updated status on demonstrations activities	accepted	15'	confirmed	Mr. Philippe Cloutet	Herakles, Safran group	France
2		Analysis of Pressure Spikes in Large Segmented Solid Rocket Booster Motor	accepted	15'	no-show	Mr. KIRAN PINUMALLA	Vikram Sarabhai Space Centre, Thiruvananthapuram-695 022, INDIA	India
3		Evaluations of Data Reduction Methods for Hybrid Rockets	accepted	15'	confirmed	Prof. Harunori Nagata	Hokkaido University	Japan
4		Small solid and hybrid thrusters development for trajectory correction on upper stage and spacecrafts	accepted	15'	no-show	Mr. Florin Mingireanu	Romanian Space Agency (ROSA)	Romania
5		Alternative Thrust Modulation Techniques for Solid and Hybrid Rockets	accepted	15'	confirmed	Dr. David Greatrix	Ryerson University	Canada
6		Hybrid Paraffin-based Technology Demonstrator in the Framework of the Italian Hyprob Program: Status of Design and Development Activities	accepted	15'	withdrawn	Mr. Francesco Ferrigno	Centro Italiano Ricerche Aerospaziali	Italy
7		Hybrid CubeSat Propulsion System with Application to a Mars Aerocapture Demonstration Mission	accepted	15'	confirmed	Ms. Elizabeth Jens	Stanford University	United States
8		development of high performance hybrid rocket engine with multi-section swirl injection method for space propulsion system	accepted	15'	confirmed	Mr. Kengo Ohe	Kyushu University	Japan
9		An Advanced Hybrid Rocket Engine for an Alternative Upper Stage of the Brazilian VLM 1 LEO-Launcher	accepted	15'	confirmed	Dr. Ognjan Bozic	Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR)	Germany
10		Benefits of a hybrid propulsion system utilizing in situ produced oxidizer for a Mars Ascent Vehicle	accepted	15'	withdrawn	Dr. Ashley Karp	Jet Propulsion Laboratory - California Institute of Technology	United States
11		Numerical Simulation and Experimental Testing on Segmented Grain Hybrid Rocket Motor	accepted	15'	no-show	Mr. Pengfei Wang	Beijing University of Aeronautics and Astronautics (BUAA)	China
12		theoretical and experimental investigation of multiple catalyst ignition of hydrogen peroxide hybrid rocket motor	accepted	15'	withdrawn	Mr. Sheng Zhao	Beijing University of Aeronautics and Astronautics (BUAA)	China
–		investigation of ignition transient process inside a longitudinal solid propellant crack	accepted	15'	withdrawn	Prof. Bing Sun	Beijing University of Aeronautics and Astronautics (BUAA)	China