session P

Title: Poster Session
type: poster
Date: 2014-10-01
Time: 13:15
Room: Prefunction

papers
Order	Paper title	Presentation status	Speaker	Affiliation	Country
1	Patent Analysis and Development Study on Airframe and Engine Integration Technology of the Aerospace Plane	withdrawn	Dr. Ping Li	China Aerospace Science and Industry Corporation	China
2	dynamics analysis for the gimballing installation of the lox/kerosene rocket engine		Dr. Fu Ping	Xi'an Aerospace Propulsion Institute	China
3	INCREASE OF EFFICIENCY OF METEROLOGICAL ROCKETS AT APPLICATION OF HYBRID MOTORS	confirmed	Mr. Kyrylo Oriekhov	Yuzhnoye State Design Office	Ukraine
4	design and preliminary characterization of a dual-mode hall thruster prototype		Mr. Le Yang	Lanzhou Institute of Physics	China
5	Research and Development of LIPS-300 Ion Thruster		Mr. liang wang	Lanzhou Institute of Physics, Electric Propulsion Department	China
6	Isolating Excited Nitrous Oxide Energy States to Enhance Dissociation	withdrawn	Mr. Pratik Saripalli	University of Maryland, College Park	United States
7	LINEAR REACTIVE ENGINE WITH ACTIVE CONTROL OF A CRITICAL SECTION AND WITH A MULTI-TIERED ARRANGEMENT OF COMBUSTION CHAMBERS	withdrawn	Mr. Oleg Aleksandrov		United States
8	Research on the High Frequency Combustion Instability in the Model of LOX/Kerosene Rocket Engine	withdrawn	Ms. Yongjing Ga	Beijing Institute of Aerospace Systems Engineering	China
9	10000 hours orificed lanthanum hexaboride hollow cathode life test	withdrawn	Dr. Ning GUO	Lanzhou Institute of Physics	China
10	Life Time Evaluation of Reusable Film-cooling Jacket of Ramjets Under Thermal Shock Condition		Mr. ren jiawan		China
11	3rd generation electric propulsion drive	withdrawn	Dr. Robert Sheldon		United States
12	Viscoplastic thermal ratcheting analysis of the reusable rocket thrust chamber wall	confirmed	Ms. Jinhui Yang	Beihang University	China
13	reusable rocket engine system design and optimization		Dr. Tao Chen	Beihang University	China
15	Solar Occulter Application to Extra-Solar Sundiver Missions	confirmed	Prof. Gregory Matloff	New York City College of Technology	United States
16	Performance analysis of a Hybrid rocket for the first stage of the VEGA launcher	withdrawn	Dr. Antonella Ingenito	University of Rome “La Sapienza”	Italy
17	Pulsed resistojet thruster with power delivery system based on supercapacitors	withdrawn	Dr. Lukasz Mezyk	Warsaw University of Technology (WUT)	Poland
18	conceptual design of an upper-stage paraffin-based hybrid propulsion system	confirmed	Ms. Praskovia Milova	Politecnico di Milano	Italy
19	The configuration design and optimize of an efficient platelet heat exchanger used in solar thermal propulsion		Mr. XING Baoyu	National University of Defense Technology	China
20	Fluid-solid Coupled Heat Transfer and Flow Simulation of Platelet Heat Exchanger in Solar Thermal Thruster		Mr. XING Baoyu	National University of Defense Technology	China
21	Systems for Spacecraft Propulsion in Both Atmospheric and Deep Space Conditions	withdrawn	Ms. Catherine Kari Derow		United Kingdom
23	Space Propulsion Using Kinetic Energy		Mr. David Callahan		United States
24	VASIMR(R) VX-CR: Status and characterization upon upgrade of its magnetic configuration	withdrawn	Dr. Jose Antonio Castro Nieto	Ad Astra Rocket Company	Costa Rica
25	research progresses on green propulsion technology for han-based propellant	confirmed	Mr. xin Qiu	Shanghai Institute of Space Propulsion	China
26	Reaction Control System Using Hybrid Micro-Thrusters, Model and Experiment	confirmed	Prof. Teodor-Viorel Chelaru	University POLITEHNICA of Bucharest - Research Center for Aeronautics and Space	Romania
27	Engines for advanced launch-vehicles of heavy and super-heavy classes	confirmed	Mr. Vladimir Sudakov	JSC NPO Energomash	Russian Federation
28	LOX-kerosene LPRE with supply of polymer additives to reduce hydro losses in fuel lines (additional study)	withdrawn	Mr. Vladimir Sudakov	JSC NPO Energomash	Russian Federation
29	System of functional diagnostics of LPRE	confirmed	Mr. Vladimir Sudakov	JSC NPO Energomash	Russian Federation
30	KEY ISSUES OF CREATING A CLOSED CYCLE LRE WITH DEEP THRUST THROTTLING	confirmed	Mr. Volodymyr Shulga	Yuzhnoye State Design Office	Ukraine
31	Mission Design study of an RTG powered Ion Engine equipped Interstellar spacecraft	confirmed	Mr. Joshua Fogel	University of Southern California	United States
32	alternative approach on calibration of micronewton thrust stand using commercial heat sink		Mr. zirui lau	Nanyang Technological University	Singapore, Republic of
33	Initiation and stabilization of oblique detonation wave in a supersonic wind tunnel	confirmed	Dr. Yu Liu	Science and Technology on Scramjet Laboratory, National University of Defense Technology	China
34	numerical simulation of satellite charging for electromagnetic orbital control	confirmed	Mr. Kento Hoshi	Kyoto University	Japan
35	Development of a CFRP based Vacuum Arc Thruster for a Nano-Satellite HORYU-IV	confirmed	Mr. Shingo Fuchikami	Kyushu Institute of Technology	Japan
36	inspection in life critical components and maintainability of reusable sounding rocket engine	confirmed	Dr. Masaki Sato	Japan Aerospace Exploration Agency (JAXA)	Japan
37	project bair: black hole augmented interstellar ramjet	confirmed	Mr. Andrew Alexander	International Space University (ISU)	United States
38	airframe-engine optimization for ramjet/scramjet along fight trajectory	withdrawn	Dr. Jisong Zhao	Northwestern Polytechnical University	China
39	A Water-Fed Micro-Resistojet for the DelFFi Formation Flying Mission	confirmed	Mr. Rob Poyck	Delft University of Technology (TU Delft)	The Netherlands
40	Thrust chamber modeling for system analysis of Liquid Rocket Engines	withdrawn	Mr. Marco Leonardi	University of Rome "La Sapienza"	Italy
41	research on radiation heat transfer of nozzle inner face	confirmed	Mrs. weijing zhang		China
42	Numerical analysis of the self-pressurization in a cryogenic storage tank	withdrawn	Ms. Juan Fu	National University of Defense Technology	China
43	The Current Status For Crew Waste Water Electrical Propulsion System by Using Arcjet Thruster	withdrawn	Mr. Yuichiro Nogawa	Japan Aerospace Exploration Agency (JAXA)	Japan
44	study on surface waves of the liquid jet in a mach 2.1 crossflow		Dr. Liyin Wu	Science and Technology on Scramjet Laboratory, National University of Defense Technology	China
45	Adjoint-Based Small Solid Rocket Motor Optimization Tool		Mr. Florin Mingireanu	Romanian Space Agency (ROSA)	Romania
46	Low cost solid rocket motor for supersonic test vehicle		Mr. Florin Mingireanu	Romanian Space Agency (ROSA)	Romania
47	Enhanced Solid Propellant Burn Rate Measurement Technique Using X-Ray Real-Time Radiography	withdrawn	Mr. Ali Butt	University of Alabama in Huntsville	United States
48	Numerical study on detonation initiation by shock wave via over-expansion in a supersonic premixed flow	confirmed	Dr. Yu Liu	Science and Technology on Scramjet Laboratory, National University of Defense Technology	China
49	System Analysis Program of Liquid Propulsion System for Launch Vehicle		Mr. Sangbok Lee	Inha Univ.	Korea, Republic of
50	design and experimental investigation of RBCC engine operating from Mach 2.0 to 6.0	confirmed	Mr. Chunqin Luo	Science and Technology on Scramjet Laboratory, Beijing Power Machinery Research Institute	China
51	numerical simulation of a single hydrazine droplet burning with a detailed kinetic mechanism	withdrawn	Dr. Kaori Ohminami	Yale University	United States
52	Low-Cost Solid Rocket Motor Development	confirmed	Mr. Adam Okninski	Institute of Aviation	Poland
53	Investigation on the Feasibility of Using Oxidizer Liquid Film Cooling for a Bipropellant Orbit and Attitude Control Rocket Engine	confirmed	Mr. Feng Zhang	Xi'an Aerospace Propulsion Institute	China
54	Instability of Cryogenic Swirl Flows under Supercritical Conditions	confirmed	Mr. Seongho Cho	Seoul National University	Korea, Republic of
55	design, manufacture, tests and evaluation of a paraffin fueled hybrid rocket motor with sequential and uninterrupted burn with oxidants air and oxygen		Mr. Thiago Barros	Instituto Tecnológico de Aeronáutica (ITA)	Brazil
56	multi-objective optimization design of RBCC ejector mode performance	confirmed	Dr. yuntao zheng	Science and Technology on Scramjet Laboratory, Beijing Power Machinery Research Institute	China
57	Helicon Plasma Electric Propulsion with ADN Propellant		Prof. Zhao Hua	China Academy of Space Technology (CAST)	China
58	experimental characterization and performance analysis of low power arcjet thrusters operated on argon, nitrogen and ammonia	withdrawn	Dr. Yingchao Xiao	Beihang University	China
59	numerical simulation of arc-heated non-ideal electromagnetic fluid trans-supersonic flow by nnd spatial discretization scheme	withdrawn	Dr. Yingchao Xiao	Beihang University	China
60	Effect of Surface Contamination on Ignition Transient in Solid Boosters	confirmed	Mr. khadar voli	Indian Space Research Organization (ISRO)	India
61	DESIGN OF HYBRID ROCKET CONTROL SYSTEM	withdrawn	Dr. song jia	Beihang University	China
62	on the role of surface orientation in relation to regression rates		Mr. Pratik Tiwari	SRM University Chennai	India
63	The Effect of Magnetic Field on The Performance of The Ion Thruster Discharge Chamber	confirmed	Dr. JuanJuan Chen	Lanzhou Institute of Physics	China

session P

Order

Time

Paper title

Mode

Presentation status

Speaker

Affiliation

Country