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: 2015-10-12
Time: 15:15
Room: Ballroom B (Crowne Plaza Hotel, -1 floor)

IPC members

Co-Chair: Mr. Christophe Bonhomme, Centre National d'Etudes Spatiales (CNES), France;
Co-Chair: Mr. Patrick Danous, ArianeGroup, France;
Rapporteur: Dr. Vanniyaperumal Narayanan, Indian Space Research Organization (ISRO), India;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1		The Development Plan of the First and the Second Stage Engines for the Japanese Next Flagship Launch System	15'	withdrawn	Mr. Shusuke Hori	Japan Aerospace Exploration Agency (JAXA)	Japan
2		Creation of family of LPRE for advanced Russian and foreign launch-vehicles on the basis of RD191 engine	15'	confirmed	Mr. Petr Levochkin	JSC NPO Energomash	Russian Federation
2		Creation of family of LPRE for advanced Russian and foreign launch-vehicles on the basis of RD191 engine	15'	confirmed	Mr. Vladimir Sudakov	JSC NPO Energomash	Russian Federation
3		Advancement and Future Application of Space Propulsion Technology Using Hydrocarbon Propellants in China	15'	confirmed	Mr. LI Wenlong	Xi'an Aerospace Propulsion Institute	China
4		The Future of Liquid Propulsion: the French view	15'	confirmed	Mr. Christophe Bonhomme	Centre National d'Etudes Spatiales (CNES)	France
5		Results of LE-X engine technology demonstration	15'	withdrawn	Mr. Hideto Kawashima	JAXA	Japan
6		VINCI®, the European reference for Ariane 6 upper stage cryogenic engine	15'	confirmed	Mr. Patrick Danous	Snecma	France
7		Development of a LM10-MIRA LOX – LNG expander cycle Demonstrator engine	15'	confirmed	Mr. Daniele Liuzzi	Avio Spa	Italy
8		firing tests for advanced features and long-life durability of the main engine of the reusable sounding rocket	15'	confirmed	Dr. Toshiya Kimura	Japan Aerospace Exploration Agency (JAXA)	Japan
9		Applying a Mature Green Propulsion Solution to Enhance Future Mission Capabilities	15'	confirmed	Ms. Elizabeth Driscoll	Aerojet Rocketdyne	United States
10		A Novel Green Gel Propellant Based Propulsion System	15'	withdrawn	Prof. Benveniste Natan	Technion – Israel Institute of Technology	Israel
11		Research on thermal decomposition of hydrogen peroxide.	15'	confirmed	Dr. Lukasz Mezyk	Warsaw University of Technology (WUT)	Poland
12		Dynamic characteristics of open-type swirl injector with pulsating manifold pressure	15'	confirmed	Mr. Yunjae Chung	Seoul National University	Korea, Republic of
13		a review of china's lox/kerosene stage combustion cycle rocket engine	15'	confirmed	Prof. Chen Jianhua	Xi'an Aerospace Propulsion Institute	China
14		Features of the propellant tanks pressurization systems development of the LV upper stages	15'	confirmed	Mr. Vadym Khomyak	Yuzhnoye State Design Office	Ukraine