session P

Title: Poster Session
type: poster
Date: 2013-09-25
Time: 13:30
Room: North Foyer

IPC members

Co-Chair: Dr. John M. Horack, The Ohio State University College of Engineering, United States;
Co-Chair: Mr. Ulf Palmnäs, Swedish Space Corporation (SSC), Sweden;

papers
Order	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	Experimental study on the high-pressure gas flow performance of orifice plates used in the rocket propellant pressurization system	Poster	confirmed	Mr. Wang Huilong	Beijing Aerospace Institute of Metrology & Measurement Technology	China
2	visualization technology of numerical simulation for launch vehicle during flight	Poster	confirmed	Dr. Zhenhai Wanyan	Beijing institute of Astronautical Systems Engineering, Beijing	China
3	a possibility based mission design optimization for the space launch vehicle	Poster	confirmed	Mr. JUNG-IL SHU	Konkuk University	Korea, Republic of
4	Experimental Research on Simulation of Rockets Takeoff	Poster	confirmed	Mr. fuyou huang		China
5	A New Optics and Radar Strap-down Measuring System	Poster	confirmed	Dr. Jiahong Chen		China
6	Research on Fast Testing Methos of Launch Vehicle	Poster	confirmed	Mr. Ziyu Wang	Beijing Institute of Aerospace Systems Engineering, China Aerospace Science and Technology Corporation (CASC)	China
7	Adaptive Fault-tolerant Control System of Reusable Launch Vehicle	Poster	confirmed	Ms. Xin Zhang	Harbin Institute of Technology	China
8	development of a linear sweeping frequency pressure generator for dynamic pressure calibration	Poster	confirmed	Mr. Dayou Zhang		China
9	water suppression test on jet noise	Poster	confirmed	Prof.Dr. Chen Jinsong	China Academy of Launch Vehicle Technology, China	China
10	Stable tracking of Narrow-beam Instrumentation Radar of Space Tracking Ship	Poster	confirmed	Mr. Qu Yuanxin		China
11	An analytical for the designing of general assembly-test building of spacecraft launch site	Poster	confirmed	Mr. Xian Feng	CAST	China
12	the analysis about the developing approaches of technologies of safely recycling and reusing launch vehicle core stages and rocket boosters	Poster	confirmed	Mr. Shang Xianyang	China Academy of Launch Vehicle Technology (CALT)	China
13	Aerodynamic analysis of the USV3 vehicle from hypersonic to landing flight conditions	Poster	confirmed	Dr. Francesco Petrosino	CIRA Italian Aerospace Research Centre	Italy
14	Orbital transfer transport system base on upper stage technology	Poster	confirmed	Mr. Xubin Zhang	China Aerospace Science and Technology Corporation (CASC)	China
15	Multi-disciplinary design and trajectory optimisation of a Single-Stage-to-Orbit Vehicle	Poster	confirmed	Mr. Romain Wuilbercq	University of Strathclyde	United Kingdom
16	FEASIBILITY STUDY OF SPACECRAFT CLUSTER LAUNCHES WITH ONE LAUNCH VEHICLE INTO VARIOUS BASIC ORBITS	Poster	confirmed	Mr. Igor Mashtak	Yuzhnoye State Design Office	Ukraine
17	Rockoon LEEM Project	Poster		Mr. Daniel Pastor Moreno	UPM-LEEM	Spain
18	A Framework for Integrating Different Space Launch Concepts for Efficient Space Launch Operations	Poster	withdrawn	Mr. Seyed Ali Nasseri	University of Toronto Institute for Aerospace Studies	Canada
19	the solution of future space transport—the patent analysis of 3dp technology application in aerospace	Poster	confirmed	Mr. Li Feng	China Aerospace Science & Industry Academy	China
20	Aerothermodynamics of round leading edge airfoil with a flow-through duct at hypersonic speed	Poster		Mr. Rajesh Yadav	University of Petroleum and Energy Studies	India
21	Vacuum Maglev - a greener and sustainable space transport system that could kick-start further international collaboration.	Poster	confirmed	Dr. Tanay Sharma	University of Sussex	United Kingdom
22	Research on the Integration of Small Launch Vehicle and Small Satellite Platform	Poster	confirmed	Mr. ChangWei Hu		China
23	A Balloon Based Launch System for Micro/Nano/Pico-Satellites	Poster	withdrawn	Mr. Seyed Ali Nasseri	University of Toronto Institute for Aerospace Studies	Canada
24	The Control System Simulation of New Launch Vehicle Based on HLA	Poster	confirmed	Dr. Guangping Qi	Beijing Aerospace Automatic Control Institute	China
25	Manned Lunar Launching Mode and the Requirement for Heavy LAUNCH Vehicle	Poster	confirmed	Ms. Wenqing Li	China Academy of Launch Vehicle Technology(CALT)	China
26	study of a new aerospace vehicle project based on turbine-based combined cycle engine	15'	confirmed	Dr. xin xu	Beijing Institute of Mechanical & Engineering	China

session P

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