session P

Title

Poster Session

Date

2013-09-25

Time

13:30

Room

North Foyer

IPC members
papers

Order

Time

Paper title

Selection result

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

accepted

Poster

confirmed

Mr. Wang Huilong

Beijing Aerospace Institute of Metrology & Measurement Technology

China

2

visualization technology of numerical simulation for launch vehicle during flight

accepted

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

accepted

Poster

confirmed

Mr. JUNG-IL SHU

Konkuk University

Korea, Republic of

4

Experimental Research on Simulation of Rockets Takeoff

accepted

Poster

confirmed

Mr. fuyou huang

China

5

A New Optics and Radar Strap-down Measuring System

accepted

Poster

confirmed

Dr. Jiahong Chen

China

6

Research on Fast Testing Methos of Launch Vehicle

accepted

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

accepted

Poster

confirmed

Ms. Xin Zhang

Harbin Institute of Technology

China

8

development of a linear sweeping frequency pressure generator for dynamic pressure calibration

accepted

Poster

confirmed

Mr. Dayou Zhang

China

9

water suppression test on jet noise

accepted

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

accepted

Poster

confirmed

Mr. Qu Yuanxin

China

11

An analytical for the designing of general assembly-test building of spacecraft launch site

accepted

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

accepted

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

accepted

Poster

confirmed

Dr. Francesco Petrosino

CIRA Italian Aerospace Research Centre

Italy

14

Orbital transfer transport system base on upper stage technology

accepted

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

accepted

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

accepted

Poster

confirmed

Mr. Igor Mashtak

Yuzhnoye State Design Office

Ukraine

17

Rockoon LEEM Project

accepted

Poster

Mr. Daniel Pastor Moreno

UPM-LEEM

Spain

18

A Framework for Integrating Different Space Launch Concepts for Efficient Space Launch Operations

accepted

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

accepted

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

accepted

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.

accepted

Poster

confirmed

Dr. Tanay Sharma

University of Sussex

United Kingdom

22

Research on the Integration of Small Launch Vehicle and Small Satellite Platform

accepted

Poster

confirmed

Mr. ChangWei Hu

China

23

A Balloon Based Launch System for Micro/Nano/Pico-Satellites

accepted

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

accepted

Poster

confirmed

Dr. Guangping Qi

Beijing Aerospace Automatic Control Institute

China

25

Manned Lunar Launching Mode and the Requirement for Heavy LAUNCH Vehicle

accepted

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

accepted

15'

confirmed

Dr. xin xu

Beijing Institute of Mechanical & Engineering

China