IAF Digital Library

3

session 3

Title: Propulsion Technology (1)
Description: This session included all science and technologies supporting all aspects of space propulsion. The emphasis in this session is plased in particular components for propulsion.
Date: 2015-10-14
Time: 09:45
Room: Ballroom B (Crowne Plaza Hotel, -1 floor)

IPC members

Co-Chair: Mr. Didier Boury, ArianeGroup SAS, France;
Co-Chair: Dr. Angelo Cervone, Delft University of Technology (TU Delft), The Netherlands;
Rapporteur: Mr. John Harlow, Aerojet Rocketdyne, United Kingdom;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1		jet inducer for a turbo pump of a liquid rocket engine	15'	confirmed	Mr. Wolfgang Kitsche	German Aerospace Center (DLR)	Germany
2		Engine Control System for the Main Engine of the Reusable Sounding Rocket	15'	confirmed	Mr. Takeshi Kai	Mitsubishi Heavy Industries, Ltd.	Japan
3		New horizons for SMA (Shape Memory Alloy) in Space Propulsion Applications	15'	confirmed	Mr. OFER LIVNE	Rafael Advanced Defense Systems Ltd.	Israel
4		In flight achievements and follow-on for Cold Gas Micro Propulsion applied to S/C Fine Pointing and Attitude Control G.Noci A.Polli	15'	confirmed	Dr. Giovanni Enrico Noci	Selex ES	Italy
5		Overview of NASA’s Green Propellant Infusion Mission and NASA Glenn Research Center’s Thruster Testing and Plume Diagnostics	15'	confirmed	Mr. Timothy Smith	NASA	United States
6		The Italian LOX/LCH4 rocket engine technology demonstrator: achievements and outlook	15'	no-show	Dr. Daniele Ricci	CIRA Italian Aerospace Research Center, Capua	Italy
7		rafael passivation valve for satellites propulsion system	15'	confirmed	Mr. Michael Zaberchik	Rafael Advanced Defense Systems Ltd.	Israel
8		cold Gas Propulsion system for the samson nano satellites	15'	confirmed	Mr. Michael Zaberchik	Rafael Advanced Defense Systems Ltd.	Israel
9		Assessment of various fuel additives for reliable hypergolic ignition with 98+ HTP	15'	confirmed	Mr. Wojciech Florczuk	Institute of Aviation	Poland
10		Analysis of Infrared Signature of Spacecraft propulsion Plume	15'	no-show	Dr. Jianwei LU	China Academy of Launch Vehicle Technology (CALT)	China
11		numerical simulation study on combustion performance of low thrust LOX/methane rocket engine	15'	confirmed	Prof. Shen Chibing	National University of Defense Technology	China
12		Preliminarily Microexplosion Model of Organic-Gellant Gel Fuel Droplets	15'	withdrawn	Dr. Zejun Liu	PLA Information Engineering University	China
13		influence of retractive length of coaxial injector on high-frequency combustion instability for staged combustion lox/kerosene rocket engine	15'	no-show	Mr. Longfei Li	Xi'an Aerospace Propulsion Institute	China
14		Dynamic Calculation Model for an Attitude Control System that uses Tilting Nozzles	15'	confirmed	Mr. Adrian Danciu	University POLITEHNICA of Bucharest - Research Center for Aeronautics and Space	Romania