IAF Digital Library

3

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 posed in particular on components for propulsion.
Date: 2011-10-05
Time: 10:00
Room: TS-06

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	Mode	Presentation status	Speaker	Affiliation	Country
1		A New Fabrication Route for Ceramic MEMS-based Micropropulsion System - Soft Molding Technique using Submicron Alumina particles and Preceramic Polymer	20	confirmed	Mr. Kean How Cheah	University of Nottingham Malaysia Campus	Malaysia
2		A SILICON-BASED MEMS RESISTOJET FOR PROPELLING CUBESATS	20	confirmed	Mr. Tittu Varghese Mathew		Switzerland
3		Development of a nitrous oxide monopropellant micro-thruster at buaa: 2010	20	confirmed	Prof. Guobiao Cai	Beijing University of Aeronautics and Astronautics (BUAA)	China
4		Safety Evaluation of Hydroxyl Ammonium Nitrate(HAN) Based Monopropellants for Thrusters	15	confirmed	Mr. Nobuyuki Azuma	Japan Aerospace Exploration Agency (JAXA)	Japan
5		LASER IGNITION OF ROCKET PROPELLANTS	15	withdrawn	Prof. Sergey Rebrov	Keldysh Research Center	Russian Federation
6		Paraffin-Based Hybrid Rocket Testing At The Butte AeroTec Facility	15	confirmed	Mr. David Micheletti		United States
7		Hot testing of laser welded channel wall nozzles on Vulcain 2 Engine and subscale stage combustion demo	15	confirmed	Mr. Ulf Palmnäs	GKN Aerospace Engine Systems	Sweden
8		Analysis of Thruster Exhaust Plume Impingement on Flexible Membrane of Solar Sail “IKAROS”	15	confirmed	Mr. Norizumi Motooka	University of Tokyo	Japan
9		Research on the Radial Turbine Used in the LOX/Hydrogen Rocket Engine	15	no-show	Mr. ZhongXiang Liu	Beijing Aerospace Propulsion Institute	China
10		Experimental and analytical characterization of shear coaxial GO2/GCH4 injector combustion flowfield	15	confirmed	Dr. Yushan Gao	Beijing University of Aeronautics and Astronautics (BUAA)	China
11		Effective Stability Analysis of Liquid Rocket Combustion Chambers: Experimental Investigation of Damped Admittances	15	confirmed	Mr. Thomas Fiala	Technische Universität München	Germany
12		Methane based hybrid rocket motor. Oxidizer doping model	15	confirmed	Mr. Florin Mingireanu	Romanian Space Agency (ROSA)	Romania