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, Italian Space Agency (ASI), Italy;

papers
Order	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	The Research on the Principle of EMdrive Propulsion Technology	Poster		Dr. Chen Yue		China
2	LOX-kerosene liquid rocket engine with a thrust of 9.8 MN	Poster	confirmed	Mr. Dmitriy Pushkarev	JSC NPO Energomash	Russian Federation
3	Start-up Transient Simulation of 60t Class LOX/Methane Liquid Rocket Engine	Poster	confirmed	Mr. WANG JUN	Beijing Aerospace Propulsion Institute	China
4	Numerical Simulation for the Satellite Propulsion System	Poster	confirmed	Ms. Duan Na	Beijing Institute of Aerospace Testing Technology	China
5	The comparison of combustion characteristics between oxygen/methane and oxygen/propane for bipropellant thruster	Poster	withdrawn	Mr. Byeongseob Park	Korea Advanced Institute of Science and Technology (KAIST)	Korea, Republic of
6	characterisation and electrolytic decomposition of adn-han mixture in a polymer micropropulsion system	Poster		Dr. Jit Kai Chin	University of Nottingham Malaysia Campus	Malaysia
7	the influence of nitrogen pressurization of liquid oxygen quality	Poster	confirmed	Mr. ZHANG JIAXIAN	Beijing Institute of Aerospace Testing Technology	China
8	cfd modeling activities on testing technology of liquid rocket engine	Poster	confirmed	Dr. Mao Li	Beijing Institute of Aerospace Testing Technology	China
9	Oxygen and methane liquid propellant rocket engines for reusable space transport system	Poster	confirmed	Dr. Igor Fatuev	NPO Energomash	Russian Federation
10	ANALYTICAL STUDY RESULTS OF GREEN PROPELLANT APPLICATION POSSIBILITY IN LANDING MODULE AND SPACE TUG ENGINES	Poster	confirmed	Mr. Andrew Kukhta	Yuzhnoye State Design Office	Ukraine
11	Developing Tendency in Liquid Rocket Engine Research and Corresponding Key Technologies	Poster	confirmed	Dr. Li Bin	Xi'an Aerospace Propulsion Institute	China
12	The service life assessment of NEPE propellant	Poster		Dr. xie hongyu		China
13	Mechanical behavior research for air-ground inconsistency of solid rocket motor	Poster		Mr. wang yongping	The 41st Institute of the Sixth Academy of Aerospace Science & Industry Corp	China
14	solid rocket motor segment dismantling, cause analysis and reassembly	Poster	confirmed	Mr. balabadra mahesh	Defence Research & Development Laboratory (DRDL)	India
15	ultrasonic measurement of solid fuel regression rate of a hybrid slab motor	Poster	confirmed	Mr. Sheng Zhao	Beijing University of Aeronautics and Astronautics (BUAA)	China
16	Design and performance evaluation of lab-scale hybrid thruster using catalytically decomposed hydrogen peroxide oxidizer	Poster	confirmed	Mr. Minwoo Lee	Korea Advanced Institute of Science and Technology (KAIST)	Korea, Republic of
17	Numerical Simulation and Testing of H2O2 - LDPE Hybrid Rocket Motor with Diaphragm	Poster	confirmed	Mr. Pengfei Wang	Beijing University of Aeronautics and Astronautics (BUAA)	China
18	Experimental Investigation on Combustion of Aluminum in the AP/HTPB Composite Propllent	Poster	confirmed	Mr. Xin Liu	Northwestern Polytechnical University	China
19	Transient Simulation of Operation Process in a Throttleable Hybrid Rocket Motor	Poster	confirmed	Mr. Peng Zeng	Beijing University of Aeronautics and Astronautics (BUAA)	China
20	biglobal instability of compressible taylor-culick flow	Poster	confirmed	Mr. Shangrong YANG	Northwestern Polytechnical University	China
21	The comparison of the different models of the burning regression rate in the hybrid rocket motor	Poster		Dr. Valery Bucharsky	Dnepropetrovsk National University named after Oles' Gonchar	Ukraine
22	Replacement of hydrazine-based systems by means of hybrid rockets	Poster	withdrawn	Dr. Filippo Maggi	Politecnico di Milano	Italy
23	experimental investigation of fuel regression rate in HTPB based lab-scale hybrid rocket motor	Poster	confirmed	Mr. Xintian Li	Beihang University	China
24	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	Poster		Mr. JOHN VIVIAN PRASHANT	Indian Space Research Organization (ISRO)	India
25	Design and simulation of gas oxygen / methane vortex cooling thrust chamber	Poster	confirmed	Mr. Gongnan Li	Beijing University of Aeronautics and Astronautics (BUAA)	China
26	Viscoplastic and elasto-plastic thermal-structure analysis of the reusable rocket thrust chamber	Poster		Ms. Jinhui Yang	Beihang University	China
27	The TVC Systems for a Chinese Liquid Oxygen and Kerosene Launch Vehicle	Poster	confirmed	Mr. Shoujun Zhao	China Academy of Launch Vehicle Technology (CALT)	China
28	Heat Exchange and Pressure Drop induced by Sloshing	Poster	withdrawn	Prof.Dr. Takehiro Himeno	University of Tokyo	Japan
29	Research on the scheme and hot fire tests of combustion devices for 100kN LOX/methane rocket engine	Poster		Mrs. Ma Dongying	Xi'an Aerospace Propulsion Institute	China
30	development of fluid control components for liquid propulsion systems of isro	Poster		Mr. G. SUNDARAVADIVELU	LPSC, ISRO	India
31	Research of laser ignition of propellant oxygen-kerosene in the model set	Poster	confirmed	Mr. Nikolay Ivanov	JSC NPO Energomash	Russian Federation
32	Effects of electrode geometry on magnetic field distribution in a pulsed plasma thruster	Poster	confirmed	Mr. Hua Zhang	College of Aerospace Science and Engineering, National University of Defense Technology	China
33	Development of Scaling Models for Applied Field Magnetoplasmadynamic Thrusters	Poster	confirmed	Mr. Tobias Mayer	Institute of Space Systems, University of Stuttgart	Germany
34	evaluation of the performances of a helicon plasma thruster	Poster	confirmed	Mr. Cheng Yuguo	National University of Defense Technology of the Chinese People's Liberation Army	China
35	Study on the Plume characteristics of Pulsed Plasma Thruster	Poster		Dr. Rui Zhang	College of Aerospace and Materials Engineering, National University of Defense Technology	China
36	Development of a Charge Exchange Thruster for Nanosatellite Missions	Poster	confirmed	Mr. Rishi Verma		Australia
37	Design, manufacturing and characterization of a 1 milliNewton class FEEP emitter	Poster	withdrawn	Dr. Angela Rossodivita	Sitael Spa	Italy
38	Thermionic emission by a thin bare tether with low-W coating	Poster	confirmed	Ms. Xin Chen	Madrid Politechnic University	Spain
39	DEVELOPMENT AND TESTING OF THE INERTIAL ELECTROSTATIC CONFINEMENT DIFFUSION THRUSTER	Poster	confirmed	Mr. Mark Becnel	University of Alabama in Huntsville	United States
40	Experimental investigation of self-excitation influence on low frequency oscillations of SPT	Poster	confirmed	Ms. zhang wen	China Academy of Launch Vehicle Technology (CALT)	China
41	Experimental optimization of preheating duration in low-power resistojet	Poster		Mr. Abdolrahim Rezaeiha	Sharif University of Technology	Iran
42	Fabrication of self-ordered nano-scale emitters in FEEP	Poster		Dr. Liu Yuming	China Academy of Space Technology (CAST)	China
43	study of density jump phenomenon under the effect of circuit loss in a helicon plasma thruster	Poster	confirmed	Mr. Cheng Yuguo	National University of Defense Technology of the Chinese People's Liberation Army	China
44	The Dynamic Operation of a High Q EmDrive Microwave Thruster	Poster	confirmed	Mr. Roger Shawyer	Satellite Propulsion Research Ltd	United Kingdom
45	Study on the operation process of pulsed plasma thrusters by a modified electromechanical model	Poster	confirmed	Mr. Hua Zhang	College of Aerospace Science and Engineering, National University of Defense Technology	China
46	The limiting current of the ion beam in laboratory operating conditions of the Hall thruster	Poster	confirmed	Mr. Nikolay Shumilin	Moscow Institute of Electronics and Mathematics of National Research University Higher School of Economics (MIEM NRU HSE)	Russian Federation
47	Interdependence between integral characteristics of Hall thrusters	Poster	confirmed	Mr. Alexander Shumilin	Moscow Institute of Electronics and Mathematics of National Research University Higher School of Economics (MIEM NRU HSE)	Russian Federation
48	Integration Considerations in Satellite Propulsion Systems: Hall Thrusters versus Ion Engines	Poster	confirmed	Mr. Roberto Dextre		United States
49	Study and Analysis of Plume Backflow From a Lithium Magnetoplasmadynamic Thruster Enabled on an Experimental Nano-Satellite	Poster	withdrawn	Mr. Rohan M Ganapathy	Hindusthan College of Engineering and Technology	India
50	MAGNETOPLASMADYNAMIC ELECTRIC PROPULSION THRUSTER BEHAVIOR AT THE 27 MEGAWATT LEVEL – ISRO Sponsored Project	Poster	confirmed	Mr. Rohan M Ganapathy	Hindusthan College of Engineering and Technology	India
51	Effects of electrode configuration on ablative pulsed plasma thruster performance	Poster	confirmed	Mr. Hua Zhang	College of Aerospace Science and Engineering, National University of Defense Technology	China
52	investigation on wave structure and power deposition in a helicon plasma thruster	Poster	confirmed	Mr. Cheng Yuguo	National University of Defense Technology of the Chinese People's Liberation Army	China
53	Chemical structral and distribution characteristics of the Pulsed Plasma Thruster plume depostion	Poster		Dr. Rui Zhang	College of Aerospace and Materials Engineering, National University of Defense Technology	China
54	INITIAL FLIGHT TEST RESULTS OF THE LIPS-200 ELECTRIC PROPULSION SYSTEM ON SJ-9A SATELLITE	Poster	confirmed	Prof.Dr. zhang tianping	Lanzhou Institute of Physics	China
55	New thrust measurement device for 10N rocket engine	Poster	confirmed	Dr. Wanlong Liu	Beijing Institute of Aerospace Testing Technology	China
56	multiscale simulations of primary atomization for two impinging jets	Poster	confirmed	Dr. liu changbo	The 11st Institute of the Sixth Academy, China Aerospace Science and Technology Corporation (CASC)	China
57	Oxidizer-Rich Preburner-Feed System Medium Frequency Coupled Stability Investigation	Poster	confirmed	Mr. Shang Liu		China
58	Flow-induced Vibrations of Liquid Rocket Engine Bellows Subjected to Internal High Pressure and Velocity	Poster	confirmed	Dr. Fu Ping	Xi'an Aerospace Propulsion Institute	China
59	the effect of ring with large eddy simulation in the flow development cylindrical duct	Poster	withdrawn	Ms. Mon Khin Oo		Korea, Republic of
60	Investigation of Shutdown Dynamic Characteristics for LOX/Kerosene Rocket Engine	Poster		Mr. Nan Ma	Xi'an Aerospace Propulsion Institute	China
61	Microhybrid engine numerical and experimental results	Poster		Mr. Florin Mingireanu	Romanian Space Agency (ROSA)	Romania
62	space propulsion system using earths magnetic field	Poster	withdrawn	Mr. AKASH DEEP K JAIN	SRM University, kattankulathur,chennai,INDIA	India
63	The isotope Stirling power system energy management	Poster		Dr. chong xiao	China Academy of Launch Vehicle Technology (CALT)	China
64	Fusion-Fission Hybrid Pulsed Propulsion System for Improved Space Transportation	Poster		Mr. Micah Laughmiller	Univeristy of Alabama in Huntsville	United States
65	theoretical analyses of performance of the integrated rocket-ramjet engine	Poster	confirmed	Mr. QIAOFENG XIE	Warsaw University of Technology (WUT)	China
66	Investigation of Ramjet Engine Real-time Simulator Modeling and Simulating	Poster	confirmed	Mr. Junlong Liang	Northwestern Polytechnical University	China
67	wind tunnel research on forward-facing cavity flow	Poster	confirmed	Mr. Jiang Zhang	China Academy of Aerospace Aerodynamics (CAAA)	China
68	Summary and Development in Research on High-energy Laser Propulsion	Poster	confirmed	Mr. Feng QI	Beijing Institute of Aerospace Systems Engineering, China Aerospace Science and Technology Corporation (CASC)	China
69	experimental study of boron ignition and combustion in convective flow	Poster	confirmed	Mr. Chuanbo Fang	National University of Defense Technology	China
70	Analysis of Heat Release Distribution in Scramjet Combustor Using Wall Pressure Based One Dimensional Model	Poster	confirmed	Dr. Wang Chao	Science and Technology on Scramjet Laboratory, National University of Defense Technology	China
71	Experimental Investigation and Numerical Simulation on Combustion Characteristic of Solid Fuel Ramjet	Poster	confirmed	Dr. qiang xia		China
72	Numerical Investigation of a Ma 10 Stream Traced Scramjet at Off Design Conditions	Poster	confirmed	Dr. Jianxing Zhou	Beijing Mech-electro Engineering Institute, CASIC	China
73	Analysis of a combined multi-mode detonation wave engine for aerospace craft	Poster	confirmed	Dr. Kongqian Sun	Science and Technology on Scramjet Laboratory,Beijing Power Machinery Research Inst	China
74	A New Hybrid-Rocket-Based Combined-Cycle Propulsion System Concept	Poster	confirmed	Mr. Nanjia Yu	Beijing University of Aeronautics and Astronautics (BUAA)	China

session P

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