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  • session P

    Title

    Poster Session

    Date

    2013-09-25

    Time

    13:30

    Room

    North Foyer

    IPC members
    • Co-Chair: Mr. Richard Blott, British Interplanetary Society, United Kingdom;

    • Co-Chair: Mr. David Micheletti, Universal Technical Resource Services, United States;

    • Co-Chair: Mr. Giorgio Saccoccia, European Space Agency (ESA), The Netherlands;

    papers

    Order

    Presentation status

    Mode

    Paper title

    Speaker

    Affiliation

    Country

    1

    poster

    The Research on the Principle of EMdrive Propulsion Technology

    Dr. Chen Yue

    China

    2

    confirmed

    poster

    LOX-kerosene liquid rocket engine with a thrust of 9.8 MN

    Mr. Dmitriy Pushkarev

    JSC NPO Energomash

    Russian Federation

    3

    confirmed

    poster

    Start-up Transient Simulation of 60t Class LOX/Methane Liquid Rocket Engine

    Mr. WANG JUN

    Beijing Aerospace Propulsion Institute

    China

    4

    confirmed

    poster

    Numerical Simulation for the Satellite Propulsion System

    Ms. Duan Na

    Beijing institute of aerospace testing technology

    China

    5

    withdrawn

    poster

    The comparison of combustion characteristics between oxygen/methane and oxygen/propane for bipropellant thruster

    Mr. Byeongseob Park

    Korea Advanced Institute of Science and Technology (KAIST)

    Korea, Republic of

    6

    poster

    characterisation and electrolytic decomposition of adn-han mixture in a polymer micropropulsion system

    Dr. Jit Kai Chin

    University of Nottingham Malaysia Campus

    Malaysia

    7

    confirmed

    poster

    the influence of nitrogen pressurization of liquid oxygen quality

    Mr. ZHANG JIAXIAN

    Beijing institute of aerospace testing technology

    China

    8

    confirmed

    poster

    cfd modeling activities on testing technology of liquid rocket engine

    Dr. Mao Li

    Beijing institute of aerospace testing technology

    China

    9

    confirmed

    poster

    Oxygen and methane liquid propellant rocket engines for reusable space transport system

    Dr. Igor Fatuev

    NPO Energomash

    Russian Federation

    10

    confirmed

    poster

    ANALYTICAL STUDY RESULTS OF GREEN PROPELLANT APPLICATION POSSIBILITY IN LANDING MODULE AND SPACE TUG ENGINES

    Mr. Andrew Kukhta

    Yuzhnoye State Design Office

    Ukraine

    11

    confirmed

    poster

    Developing Tendency in Liquid Rocket Engine Research and Corresponding Key Technologies

    Dr. Li Bin

    Xi'an Aerospace Propulsion Institute

    China

    12

    poster

    The service life assessment of NEPE propellant

    Dr. xie hongyu

    China

    13

    poster

    Mechanical behavior research for air-ground inconsistency of solid rocket motor

    Mr. wang yongping

    The 41st Institute of the Sixth Academy of Aerospace Science & Industry Corp

    China

    14

    confirmed

    poster

    solid rocket motor segment dismantling, cause analysis and reassembly

    Mr. balabadra mahesh

    Defence Research & Development Laboratory (DRDL)

    India

    15

    confirmed

    poster

    ultrasonic measurement of solid fuel regression rate of a hybrid slab motor

    Mr. Sheng Zhao

    Beijing University of Aeronautics and Astronautics (BUAA)

    China

    16

    confirmed

    poster

    Design and performance evaluation of lab-scale hybrid thruster using catalytically decomposed hydrogen peroxide oxidizer

    Mr. Minwoo Lee

    Korea Advanced Institute of Science and Technology (KAIST)

    Korea, Republic of

    17

    confirmed

    poster

    Numerical Simulation and Testing of H2O2 - LDPE Hybrid Rocket Motor with Diaphragm

    Mr. Pengfei Wang

    Beijing University of Aeronautics and Astronautics (BUAA)

    China

    18

    confirmed

    poster

    Experimental Investigation on Combustion of Aluminum in the AP/HTPB Composite Propllent

    Mr. Xin Liu

    Northwestern Polytechnical University

    China

    19

    confirmed

    poster

    Transient Simulation of Operation Process in a Throttleable Hybrid Rocket Motor

    Mr. Peng Zeng

    Beijing University of Aeronautics and Astronautics (BUAA)

    China

    20

    confirmed

    poster

    biglobal instability of compressible taylor-culick flow

    Mr. Shangrong YANG

    Northwestern Polytechnical University

    China

    21

    poster

    The comparison of the different models of the burning regression rate in the hybrid rocket motor

    Dr. Valery Bucharsky

    Dnepropetrovsk National University named after Oles' Gonchar

    Ukraine

    22

    withdrawn

    poster

    Replacement of hydrazine-based systems by means of hybrid rockets

    Dr. Filippo Maggi

    Politecnico di Milano

    Italy

    23

    confirmed

    poster

    experimental investigation of fuel regression rate in HTPB based lab-scale hybrid rocket motor

    Mr. Xintian Li

    Beihang University

    China

    24

    poster

    The Numerical Simulation of a Staged Transverse Injection Behind a Rearward Facing Step Into a Mach 2 Stream in a Confined Environment and its application in the development of scramjet technology

    Mr. JOHN VIVIAN PRASHANT

    Indian Space Research Organization (ISRO)

    India

    25

    confirmed

    poster

    Design and simulation of gas oxygen / methane vortex cooling thrust chamber

    Mr. Gongnan Li

    Beijing University of Aeronautics and Astronautics (BUAA)

    China

    26

    poster

    Viscoplastic and elasto-plastic thermal-structure analysis of the reusable rocket thrust chamber

    Ms. Jinhui Yang

    Beihang University

    China

    27

    confirmed

    poster

    The TVC Systems for a Chinese Liquid Oxygen and Kerosene Launch Vehicle

    Mr. Shoujun Zhao

    China Academy of Launch Vehicle Technology (CALT)

    China

    28

    withdrawn

    poster

    Heat Exchange and Pressure Drop induced by Sloshing

    Prof.Dr. Takehiro Himeno

    University of Tokyo

    Japan

    29

    poster

    Research on the scheme and hot fire tests of combustion devices for 100kN LOX/methane rocket engine

    Mrs. Ma Dongying

    Xi'an Aerospace Propulsion Institute

    China

    30

    poster

    development of fluid control components for liquid propulsion systems of isro

    Mr. G. SUNDARAVADIVELU

    LPSC, ISRO

    India

    31

    confirmed

    poster

    Research of laser ignition of propellant oxygen-kerosene in the model set

    Mr. Nikolay Ivanov

    JSC NPO Energomash

    Russian Federation

    32

    confirmed

    poster

    Effects of electrode geometry on magnetic field distribution in a pulsed plasma thruster

    Mr. Hua Zhang

    College of Aerospace Science and Engineering, National University of Defense Technology

    China

    33

    confirmed

    poster

    Development of Scaling Models for Applied Field Magnetoplasmadynamic Thrusters

    Mr. Tobias Mayer

    Institute of Space Systems, Universität Stuttgart

    Germany

    34

    confirmed

    poster

    evaluation of the performances of a helicon plasma thruster

    Mr. Cheng Yuguo

    National University of Defense Technology of the Chinese People's Liberation Army

    China

    35

    poster

    Study on the Plume characteristics of Pulsed Plasma Thruster

    Dr. Rui Zhang

    College of Aerospace and Materials Engineering, National University of Defense Technology

    China

    36

    confirmed

    poster

    Development of a Charge Exchange Thruster for Nanosatellite Missions

    Mr. Rishi Verma

    Australia

    37

    withdrawn

    poster

    Design, manufacturing and characterization of a 1 milliNewton class FEEP emitter

    Dr. Angela Rossodivita

    Sitael Spa

    Italy

    38

    confirmed

    poster

    Thermionic emission by a thin bare tether with low-W coating

    Ms. Xin Chen

    Madrid Politechnic University

    Spain

    39

    confirmed

    poster

    DEVELOPMENT AND TESTING OF THE INERTIAL ELECTROSTATIC CONFINEMENT DIFFUSION THRUSTER

    Mr. Mark Becnel

    University of Alabama in Huntsville

    United States

    40

    confirmed

    poster

    Experimental investigation of self-excitation influence on low frequency oscillations of SPT

    Ms. zhang wen

    China Academy of Launch Vehicle Technology (CALT)

    China

    41

    poster

    Experimental optimization of preheating duration in low-power resistojet

    Mr. Abdolrahim Rezaeiha

    Sharif University of Technology

    Iran

    42

    poster

    Fabrication of self-ordered nano-scale emitters in FEEP

    Dr. Liu Yuming

    China Academy of Space Technology (CAST)

    China

    43

    confirmed

    poster

    study of density jump phenomenon under the effect of circuit loss in a helicon plasma thruster

    Mr. Cheng Yuguo

    National University of Defense Technology of the Chinese People's Liberation Army

    China

    44

    confirmed

    poster

    The Dynamic Operation of a High Q EmDrive Microwave Thruster

    Mr. Roger Shawyer

    Satellite Propulsion Research Ltd

    United Kingdom

    45

    confirmed

    poster

    Study on the operation process of pulsed plasma thrusters by a modified electromechanical model

    Mr. Hua Zhang

    College of Aerospace Science and Engineering, National University of Defense Technology

    China

    46

    confirmed

    poster

    The limiting current of the ion beam in laboratory operating conditions of the Hall thruster

    Mr. Nikolay Shumilin

    Moscow Institute of Electronics and Mathematics of National Research University Higher School of Economics (MIEM NRU HSE)

    Russian Federation

    47

    confirmed

    poster

    Interdependence between integral characteristics of Hall thrusters

    Mr. Alexander Shumilin

    Moscow Institute of Electronics and Mathematics of National Research University Higher School of Economics (MIEM NRU HSE)

    Russian Federation

    48

    confirmed

    poster

    Integration Considerations in Satellite Propulsion Systems: Hall Thrusters versus Ion Engines

    Mr. Roberto Dextre

    United States

    49

    withdrawn

    poster

    Study and Analysis of Plume Backflow From a Lithium Magnetoplasmadynamic Thruster Enabled on an Experimental Nano-Satellite

    Mr. Rohan M Ganapathy

    Hindusthan College of Engineering and Technology

    India

    50

    confirmed

    poster

    MAGNETOPLASMADYNAMIC ELECTRIC PROPULSION THRUSTER BEHAVIOR AT THE 27 MEGAWATT LEVEL – ISRO Sponsored Project

    Mr. Rohan M Ganapathy

    Hindusthan College of Engineering and Technology

    India

    51

    confirmed

    poster

    Effects of electrode configuration on ablative pulsed plasma thruster performance

    Mr. Hua Zhang

    College of Aerospace Science and Engineering, National University of Defense Technology

    China

    52

    confirmed

    poster

    investigation on wave structure and power deposition in a helicon plasma thruster

    Mr. Cheng Yuguo

    National University of Defense Technology of the Chinese People's Liberation Army

    China

    53

    poster

    Chemical structral and distribution characteristics of the Pulsed Plasma Thruster plume depostion

    Dr. Rui Zhang

    College of Aerospace and Materials Engineering, National University of Defense Technology

    China

    54

    confirmed

    poster

    INITIAL FLIGHT TEST RESULTS OF THE LIPS-200 ELECTRIC PROPULSION SYSTEM ON SJ-9A SATELLITE

    Prof.Dr. zhang tianping

    Lanzhou Institute of Physics

    China

    55

    confirmed

    poster

    New thrust measurement device for 10N rocket engine

    Dr. Wanlong Liu

    Beijing institute of aerospace testing technology

    China

    56

    confirmed

    poster

    multiscale simulations of primary atomization for two impinging jets

    Dr. liu changbo

    The 11st Institute of the Sixth Academy, China Aerospace Science and Technology Corporation (CASC)

    China

    57

    confirmed

    poster

    Oxidizer-Rich Preburner-Feed System Medium Frequency Coupled Stability Investigation

    Mr. Shang Liu

    China

    58

    confirmed

    poster

    Flow-induced Vibrations of Liquid Rocket Engine Bellows Subjected to Internal High Pressure and Velocity

    Dr. Fu Ping

    Xi'an Aerospace Propulsion Institute

    China

    59

    withdrawn

    poster

    the effect of ring with large eddy simulation in the flow development cylindrical duct

    Ms. Mon Khin Oo

    Korea, Republic of

    60

    poster

    Investigation of Shutdown Dynamic Characteristics for LOX/Kerosene Rocket Engine

    Mr. Nan Ma

    Xi'an Aerospace Propulsion Institute

    China

    61

    poster

    Microhybrid engine numerical and experimental results

    Mr. Florin Mingireanu

    Romanian Space Agency (ROSA)

    Romania

    62

    withdrawn

    poster

    space propulsion system using earths magnetic field

    Mr. AKASH DEEP K JAIN

    SRM University, kattankulathur,chennai,INDIA

    India

    63

    poster

    The isotope Stirling power system energy management

    Dr. chong xiao

    China Academy of Launch Vehicle Technology (CALT)

    China

    64

    poster

    Fusion-Fission Hybrid Pulsed Propulsion System for Improved Space Transportation

    Mr. Micah Laughmiller

    Univeristy of Alabama in Huntsville

    United States

    65

    confirmed

    poster

    theoretical analyses of performance of the integrated rocket-ramjet engine

    Mr. QIAOFENG XIE

    Warsaw University of Technology (WUT)

    China

    66

    confirmed

    poster

    Investigation of Ramjet Engine Real-time Simulator Modeling and Simulating

    Mr. Junlong Liang

    Northwestern Polytechnical University

    China

    67

    confirmed

    poster

    wind tunnel research on forward-facing cavity flow

    Mr. Jiang Zhang

    China Academy of Aerospace Aerodynamics (CAAA)

    China

    68

    confirmed

    poster

    Summary and Development in Research on High-energy Laser Propulsion

    Mr. Feng QI

    Beijing Institute of Aerospace Systems Engineering, China Aerospace Science and Technology Corporation (CASC)

    China

    69

    confirmed

    poster

    experimental study of boron ignition and combustion in convective flow

    Mr. Chuanbo Fang

    National University of Defense Technology

    China

    70

    confirmed

    poster

    Analysis of Heat Release Distribution in Scramjet Combustor Using Wall Pressure Based One Dimensional Model

    Dr. Wang Chao

    Science and Technology on Scramjet Laboratory, National University of Defense Technology

    China

    71

    confirmed

    poster

    Experimental Investigation and Numerical Simulation on Combustion Characteristic of Solid Fuel Ramjet

    Dr. qiang xia

    China

    72

    confirmed

    poster

    Numerical Investigation of a Ma 10 Stream Traced Scramjet at Off Design Conditions

    Dr. Jianxing Zhou

    Beijing Mech-electro Engineering Institute, CASIC

    China

    73

    confirmed

    poster

    Analysis of a combined multi-mode detonation wave engine for aerospace craft

    Dr. Kongqian Sun

    Science and Technology on Scramjet Laboratory,Beijing Power Machinery Research Inst

    China

    74

    confirmed

    poster

    A New Hybrid-Rocket-Based Combined-Cycle Propulsion System Concept

    Mr. Nanjia Yu

    Beijing University of Aeronautics and Astronautics (BUAA)

    China