IAF Digital Library

1

session 1

Title: Propulsion System (1)
type: oral
Description: This session is dedicated to all aspects of Liquid Rocket Engines.
Date: 2012-10-01
Time: 15:15
Room: TS14 (Sala Capri, Palacongressi)

IPC members

Chairman: Mr. Max Calabro, The Inner Arch, France;
Chairman: Mr. Christophe Bonhomme, Centre National d'Etudes Spatiales (CNES), France;
Rapporteur: Mr. Walter Zinner, ArianeGroup, Germany;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1		SYMPOSIUM KEYNOTE: The HYPROB Program: Mastering Key Technologies, Design and Testing Capabilities for Space Transportation Rocket Propulsion Evolution	20'	confirmed
2		DEVELOPMENT OF NEW TECHNOLOGIES APPLIED TO LOX-CH4 PROPULSION	15'	confirmed	Mr. Arione Luigi	AVIO S.p.A.	Italy
3		Demonstration of a 600kN class LOX/Methane Rocket Engine	15'	confirmed	Prof. Nan Zhang	Beijing Aerospace Propulsion Institute	China
4		Injector Conceptions for Usage of LOX/methane Propellant Composition in Liquid-Liquid, Expander and Staged Combustion Cycles of a Liquid Rocket Engine	15'	no-show	Prof. Vladimir Bazarov	Moscow Aviation Institute (State Technical University)	Russian Federation
5		OVERVIEW of LNG PROPULSION SYSTEM DEVELOPMENT	15'	confirmed	Mr. Yasuhito Kano	Japan Aerospace Exploration Agency (JAXA)	Japan
6		Main Directions of the Pneudraulic Systems Progress of Contemporary Launch Vehicles	15'	confirmed	Mr. Anatolii Lohvynenko	Yuzhnoye State Design Office	Ukraine
7		THE DEVELOPMENT AND QUALIFICATION TESTING OF THE SECOND GENERATION HIGH PERFORMANCE 490N LIQUID APOGEE ENGINE	15'	confirmed	Mr. Chnagguo Liu		China
8		Reusable Sounding Rocket Engine Design and Manufacturing Status of Development Engine and Components	15'	confirmed	Mr. Hiromichi Hiraki	Mitsubishi Heavy Industries, Ltd.	Japan
9		Progress of the development of an all-electric control system of a rocket engine	15'	confirmed	Mr. Patrick Danous	Snecma	France
10		JSC "NPO Energomash named after academician V.Glushko" - Leading Russian enterprise on the development and production of liquid propellant rocket engines. Experience and prospect.	15'	confirmed	Dr. Petr Levochkin	NPO Energomash	Russian Federation
11		Preliminary Design Study of Staged Combustion Cycle Rocket Engine for SpaceLiner High-Speed Passenger Transportation Concept	Poster	confirmed	Mr. Ryoma Yamashiro	Japan Aerospace Exploration Agency (JAXA)	Japan
12		Study on combustion characteristics according to recess length for a rocket engine using gas methane/lox as propellants	Poster	confirmed	Mr. junsu Jeon	Chungnam National University	Korea, Republic of
13		Design Optimization of Liquid Rocket Engine using a Genetic Algorithm	Poster	confirmed	Mr. Sangbok Lee	Inha Univ.	Korea, Republic of
14		Research on the cooling method for an oxygen rich preburner	Poster	withdrawn	Dr. Insang Moon	Korea Aerospace Research Institute (KARI)	Korea, Republic of
15		Development and test of the lox/lng regenerative cooled rocket engine	Poster	confirmed	Mr. Kenichi Kimoto	IHI Corporation	Japan
–		Technology Demonstration of Main Propulsion System for Reusable Sounding Rocket	with 13569		Dr. Masaki Sato	Japan Aerospace Exploration Agency (JAXA)	Japan
–		UPPER STAGE AND LANDING MODULE LIQUID ROCKET ENGINES WITH COMBINED STORABLE PROPELLANT SUPPLY SYSTEMS	with 12990	confirmed	Dr. Vladimir Shnyakin	Yuzhnoye State Design Office	Ukraine