Poster Session
2014-10-01
Order | Time | Paper title | Selection result | Mode | Presentation status | Speaker | Affiliation | Country |
---|---|---|---|---|---|---|---|---|
1 | accepted | withdrawn | Dr. Ping Li | China Aerospace Science and Industry Corporation | China | |||
2 | dynamics analysis for the gimballing installation of the lox/kerosene rocket engine | accepted | Dr. Fu Ping | Xi'an Aerospace Propulsion Institute | China | |||
3 | INCREASE OF EFFICIENCY OF METEROLOGICAL ROCKETS AT APPLICATION OF HYBRID MOTORS | accepted | confirmed | Mr. Kyrylo Oriekhov | Yuzhnoye State Design Office | Ukraine | ||
4 | design and preliminary characterization of a dual-mode hall thruster prototype | accepted | Mr. Le Yang | Lanzhou Institute of Physics | China | |||
5 | accepted | Mr. liang wang | Lanzhou Institute of Physics, Electric Propulsion Department | China | ||||
6 | Isolating Excited Nitrous Oxide Energy States to Enhance Dissociation | accepted | withdrawn | Mr. Pratik Saripalli | University of Maryland, College Park | United States | ||
7 | accepted | withdrawn | Mr. Oleg Aleksandrov | United States | ||||
8 | Research on the High Frequency Combustion Instability in the Model of LOX/Kerosene Rocket Engine | accepted | withdrawn | Ms. Yongjing Ga | Beijing Institute of Aerospace Systems Engineering | China | ||
9 | 10000 hours orificed lanthanum hexaboride hollow cathode life test | accepted | withdrawn | Dr. Ning GUO | Lanzhou Institute of Physics | China | ||
10 | Life Time Evaluation of Reusable Film-cooling Jacket of Ramjets Under Thermal Shock Condition | accepted | Mr. ren jiawan | China | ||||
11 | accepted | withdrawn | Dr. Robert Sheldon | United States | ||||
12 | Viscoplastic thermal ratcheting analysis of the reusable rocket thrust chamber wall | accepted | confirmed | Ms. Jinhui Yang | Beihang University | China | ||
13 | accepted | Dr. Tao Chen | Beihang University | China | ||||
15 | accepted | 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16 | Performance analysis of a Hybrid rocket for the first stage of the VEGA launcher | accepted | withdrawn | Dr. Antonella Ingenito | University of Rome “La Sapienza” | Italy | ||
17 | Pulsed resistojet thruster with power delivery system based on supercapacitors | accepted | withdrawn | Dr. Lukasz Mezyk | Warsaw University of Technology (WUT) | Poland | ||
18 | conceptual design of an upper-stage paraffin-based hybrid propulsion system | accepted | confirmed | Ms. Praskovia Milova | Politecnico di Milano | Italy | ||
19 | accepted | Mr. XING Baoyu | National University of Defense Technology | China | ||||
20 | accepted | Mr. XING Baoyu | National University of Defense Technology | China | ||||
21 | Systems for Spacecraft Propulsion in Both Atmospheric and Deep Space Conditions | accepted | withdrawn | Ms. Catherine Kari Derow | United Kingdom | |||
23 | accepted | Mr. David Callahan | United States | |||||
24 | VASIMR(R) VX-CR: Status and characterization upon upgrade of its magnetic configuration | accepted | withdrawn | Dr. Jose Antonio Castro Nieto | Ad Astra Rocket Company | Costa Rica | ||
25 | research progresses on green propulsion technology for han-based propellant | accepted | confirmed | Mr. xin Qiu | Shanghai Institute of Space Propulsion | China | ||
26 | Reaction Control System Using Hybrid Micro-Thrusters, Model and Experiment | accepted | 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 | accepted | confirmed | Mr. Vladimir Sudakov | JSC NPO Energomash | Russian Federation | ||
28 | accepted | withdrawn | Mr. Vladimir Sudakov | JSC NPO Energomash | Russian Federation | |||
29 | accepted | confirmed | Mr. Vladimir Sudakov | JSC NPO Energomash | Russian Federation | |||
30 | KEY ISSUES OF CREATING A CLOSED CYCLE LRE WITH DEEP THRUST THROTTLING | accepted | confirmed | Mr. Volodymyr Shulga | Yuzhnoye State Design Office | Ukraine | ||
31 | Mission Design study of an RTG powered Ion Engine equipped Interstellar spacecraft | accepted | confirmed | Mr. Joshua Fogel | University of Southern California | United States | ||
32 | alternative approach on calibration of micronewton thrust stand using commercial heat sink | accepted | Mr. zirui lau | Nanyang Technological University | Singapore, Republic of | |||
33 | Initiation and stabilization of oblique detonation wave in a supersonic wind tunnel | accepted | 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 | accepted | confirmed | Mr. Kento Hoshi | Kyoto University | Japan | ||
35 | Development of a CFRP based Vacuum Arc Thruster for a Nano-Satellite HORYU-IV | accepted | confirmed | Mr. Shingo Fuchikami | Kyushu Institute of Technology | Japan | ||
36 | inspection in life critical components and maintainability of reusable sounding rocket engine | accepted | confirmed | Dr. Masaki Sato | Japan Aerospace Exploration Agency (JAXA) | Japan | ||
37 | accepted | confirmed | Mr. Andrew Alexander | International Space University (ISU) | United States | |||
38 | airframe-engine optimization for ramjet/scramjet along fight trajectory | accepted | withdrawn | Dr. Jisong Zhao | Northwestern Polytechnical University | China | ||
39 | A Water-Fed Micro-Resistojet for the DelFFi Formation Flying Mission | accepted | confirmed | Mr. Rob Poyck | Delft University of Technology (TU Delft) | The Netherlands | ||
40 | Thrust chamber modeling for system analysis of Liquid Rocket Engines | accepted | withdrawn | Mr. Marco Leonardi | University of Rome "La Sapienza" | Italy | ||
41 | accepted | confirmed | Mr. xiaobo shi | China | ||||
42 | Numerical analysis of the self-pressurization in a cryogenic storage tank | accepted | 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 | accepted | 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 | accepted | Dr. Liyin Wu | Science and Technology on Scramjet Laboratory, National University of Defense Technology | China | |||
45 | accepted | Mr. Florin Mingireanu | Romanian Space Agency (ROSA) | Romania | ||||
46 | accepted | Mr. Florin Mingireanu | Romanian Space Agency (ROSA) | Romania | ||||
47 | Enhanced Solid Propellant Burn Rate Measurement Technique Using X-Ray Real-Time Radiography | accepted | withdrawn | Mr. Ali Butt | University of Alabama in Huntsville | United States | ||
48 | accepted | 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 | accepted | Mr. Sangbok Lee | Inha Univ. | Korea, Republic of | |||
50 | design and experimental investigation of RBCC engine operating from Mach 2.0 to 6.0 | accepted | 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 | accepted | withdrawn | Dr. Kaori Ohminami | Yale University | United States | ||
52 | accepted | confirmed | Mr. Adam Okninski | Institute of Aviation | Poland | |||
53 | accepted | confirmed | Mr. Feng Zhang | Xi'an Aerospace Propulsion Institute | China | |||
54 | Instability of Cryogenic Swirl Flows under Supercritical Conditions | accepted | confirmed | Mr. Seongho Cho | Seoul National University | Korea, Republic of | ||
55 | accepted | Mr. Thiago Barros | Instituto Tecnológico de Aeronáutica (ITA) | Brazil | ||||
56 | multi-objective optimization design of RBCC ejector mode performance | accepted | confirmed | Dr. yuntao zheng | Science and Technology on Scramjet Laboratory, Beijing Power Machinery Research Institute | China | ||
57 | accepted | Prof. Zhao Hua | China Academy of Space Technology (CAST) | China | ||||
58 | accepted | withdrawn | Dr. Yingchao Xiao | Beihang University | China | |||
59 | accepted | withdrawn | Dr. Yingchao Xiao | Beihang University | China | |||
60 | Effect of Surface Contamination on Ignition Transient in Solid Boosters | accepted | confirmed | Mr. khadar voli | Indian Space Research Organization (ISRO) | India | ||
61 | accepted | withdrawn | Dr. song jia | Beihang University | China | |||
62 | on the role of surface orientation in relation to regression rates | accepted | Mr. Pratik Tiwari | SRM University Chennai | India | |||
63 | The Effect of Magnetic Field on The Performance of The Ion Thruster Discharge Chamber | accepted | confirmed | Dr. JuanJuan Chen | Lanzhou Institute of Physics | China |