session 3

Title: Propulsion Technology
Description: This session includes all science and technologies supporting all aspects of space propulsion. The emphasis in this session is placed in particular on components for propulsion.
Date: 2012-10-03
Time: 10:15
Room: TS14 (Sala Capri, Palacongressi)

IPC members

Chairman: Mr. John Harlow, Aerojet Rocketdyne, United Kingdom;
Chairman: Mr. James Free, National Aeronautics and Space Administration (NASA), United States;
Rapporteur: Mr. Didier Boury, ArianeGroup SAS, France;

papers
Order	Time	Paper title	Selection result	Mode	Presentation status	Speaker	Affiliation	Country
1		Secondary injection thrust vectoring of an axisymmetric CD nozzle for small space launchers & vehicles	accepted	15'	confirmed	Mr. Vladeta Zmijanovic	ICARE-CNRS	France
2		Dynamics and Control of the HELIOS Solar Sail Demonstrator	accepted	15'	confirmed	Mr. Daniel Guerrant	Colorado Center for Astrodynamics Research, University of Colorado	United States
3		Research on EPDM insulation ablation by particle flow based on strength failure model for porous charring layer	accepted	15'	withdrawn	Mr. Yue Chen	Shanghai Space Propulsion Technology Research Institute	China
4		Development Of A Lox/Lch4 Technology Demonstrator Based On Regenerative Cooling Throughout Validation Of Critical Design Aspects With Breadboards In The Framework Of The Hyprob Program	accepted	15'	confirmed	Dr. Francesco Battista	CIRA Italian Aerospace Research Center, Capua	Italy
4		Development Of A Lox/Lch4 Technology Demonstrator Based On Regenerative Cooling Throughout Validation Of Critical Design Aspects With Breadboards In The Framework Of The Hyprob Program	accepted	15'	confirmed	Dr. Francesco Battista	CIRA Italian Aerospace Research Center, Capua	Italy
5		Development of Hydrogen Peroxide Rockets at Alta S.p.A.: the Past, the Present and the Future	accepted	15'	confirmed	Dr. Angelo Cervone	Delft University of Technology (TU Delft)	The Netherlands
6		Experimental Studies of the Effects of Baffles Geometry on High-frequency Combustion Instability of Liquid Rocket Engine	accepted	15'	no-show	Mr. Longfei Li	Xi'an Aerospace Propulsion Institute	China
7		A study on the improvement of ignition and thrust repeatability of a micro solid propellant thruster array	accepted	15'	confirmed	Mr. Daeban Seo	Korea Advanced Institute of Science and Technology (KAIST)	Korea, Republic of
8		Triangular Deployable Space Sail Fold Patterns and Sail Materials	accepted	15'	withdrawn	Mr. Andrew Wolahan	Cranfield University	The Netherlands
9		Ceramic Matrix Composites for Improved Rocket Engine Combustion Chambers	accepted	15'	withdrawn	Mr. David Lee	California State University, Long Beach	United States
10		Thrust dependency of microwave rocket on power density distributions of an incident millimeter wave beam	accepted	15'	confirmed	Mr. Toshikazu Yamaguchi	The University of TOKYO, Graduate school	Japan
11		Slurry-propellant rocket propulsion. New design solutions for displacing gas-generator and reliable multistart	accepted	15'	confirmed	Mr. Yulian Protsan	The Laboratory of Advanced Jet Propulsion	Ukraine
12		Reseach of the Oxidizer-Rich Preburner-Pipe System Dynamic Characteristics	accepted	15'	no-show	Mr. Shang Liu		China
13		Development of Fuel Leakage Detection Sensor In Space Propulsion System	accepted	Poster	confirmed	Ms. FUNMILAYO OGUN	National Space Research and Development Agency (NASRDA)	Nigeria
14		Hybrid Diagnostics for Spacecraft Propulsion System	accepted	Poster	confirmed	Mr. Xiaohui Peng	College of Aerospace and Materials Engineering, National University of Defense Technology	China
15		OPTIMIZATION OF ASCENT TRAJECTORY AND MASS BUDGET PREDICTION FOR A LOW POWER EXPERIMENTAL ROCKET	accepted	Poster	confirmed	Ms. Joy Amedu	National Space Research and Development Agency (NASRDA)	Nigeria
–		Development of a Liquid Oxygen-Methane Technology Demonstrator Based on Regenerative Cooling in the Framework of the HYPROB Program	merged	with 14688		Dr. Francesco Battista	CIRA Italian Aerospace Research Centre	Italy