rootbrowseIAC-14C4session PP. Poster SessionPapers1. Patent Analysis and Development Study on Airframe and Engine Integration Technology of the Aerospace Plane2. dynamics analysis for the gimballing installation of the lox/kerosene rocket engine3. INCREASE OF EFFICIENCY OF METEROLOGICAL ROCKETS AT APPLICATION OF HYBRID MOTORS4. design and preliminary characterization of a dual-mode hall thruster prototype5. Research and Development of LIPS-300 Ion Thruster6. Isolating Excited Nitrous Oxide Energy States to Enhance Dissociation7. LINEAR REACTIVE ENGINE WITH ACTIVE CONTROL OF A CRITICAL SECTION AND WITH A MULTI-TIERED ARRANGEMENT OF COMBUSTION CHAMBERS8. Research on the High Frequency Combustion Instability in the Model of LOX/Kerosene Rocket Engine9. 10000 hours orificed lanthanum hexaboride hollow cathode life test10. Life Time Evaluation of Reusable Film-cooling Jacket of Ramjets Under Thermal Shock Condition11. 3rd generation electric propulsion drive12. Viscoplastic thermal ratcheting analysis of the reusable rocket thrust chamber wall13. reusable rocket engine system design and optimization15. Solar Occulter Application to Extra-Solar Sundiver Missions16. Performance analysis of a Hybrid rocket for the first stage of the VEGA launcher17. Pulsed resistojet thruster with power delivery system based on supercapacitors18. conceptual design of an upper-stage paraffin-based hybrid propulsion system19. The configuration design and optimize of an efficient platelet heat exchanger used in solar thermal propulsion20. Fluid-solid Coupled Heat Transfer and Flow Simulation of Platelet Heat Exchanger in Solar Thermal Thruster21. Systems for Spacecraft Propulsion in Both Atmospheric and Deep Space Conditions23. Space Propulsion Using Kinetic Energy24. VASIMR(R) VX-CR: Status and characterization upon upgrade of its magnetic configuration25. research progresses on green propulsion technology for han-based propellant26. Reaction Control System Using Hybrid Micro-Thrusters, Model and Experiment27. Engines for advanced launch-vehicles of heavy and super-heavy classes28. LOX-kerosene LPRE with supply of polymer additives to reduce hydro losses in fuel lines (additional study)29. System of functional diagnostics of LPRE30. KEY ISSUES OF CREATING A CLOSED CYCLE LRE WITH DEEP THRUST THROTTLING31. Mission Design study of an RTG powered Ion Engine equipped Interstellar spacecraft32. alternative approach on calibration of micronewton thrust stand using commercial heat sink33. Initiation and stabilization of oblique detonation wave in a supersonic wind tunnel34. numerical simulation of satellite charging for electromagnetic orbital control35. Development of a CFRP based Vacuum Arc Thruster for a Nano-Satellite HORYU-IV36. inspection in life critical components and maintainability of reusable sounding rocket engine37. project bair: black hole augmented interstellar ramjet38. airframe-engine optimization for ramjet/scramjet along fight trajectory39. A Water-Fed Micro-Resistojet for the DelFFi Formation Flying Mission40. Thrust chamber modeling for system analysis of Liquid Rocket Engines41. research on radiation heat transfer of nozzle inner face42. Numerical analysis of the self-pressurization in a cryogenic storage tank43. The Current Status For Crew Waste Water Electrical Propulsion System by Using Arcjet Thruster44. study on surface waves of the liquid jet in a mach 2.1 crossflow45. Adjoint-Based Small Solid Rocket Motor Optimization Tool46. Low cost solid rocket motor for supersonic test vehicle47. Enhanced Solid Propellant Burn Rate Measurement Technique Using X-Ray Real-Time Radiography48. Numerical study on detonation initiation by shock wave via over-expansion in a supersonic premixed flow49. System Analysis Program of Liquid Propulsion System for Launch Vehicle50. design and experimental investigation of RBCC engine operating from Mach 2.0 to 6.051. numerical simulation of a single hydrazine droplet burning with a detailed kinetic mechanism52. Low-Cost Solid Rocket Motor Development53. Investigation on the Feasibility of Using Oxidizer Liquid Film Cooling for a Bipropellant Orbit and Attitude Control Rocket Engine54. Instability of Cryogenic Swirl Flows under Supercritical Conditions55. design, manufacture, tests and evaluation of a paraffin fueled hybrid rocket motor with sequential and uninterrupted burn with oxidants air and oxygen56. multi-objective optimization design of RBCC ejector mode performance57. Helicon Plasma Electric Propulsion with ADN Propellant58. experimental characterization and performance analysis of low power arcjet thrusters operated on argon, nitrogen and ammonia59. numerical simulation of arc-heated non-ideal electromagnetic fluid trans-supersonic flow by nnd spatial discretization scheme60. Effect of Surface Contamination on Ignition Transient in Solid Boosters61. DESIGN OF HYBRID ROCKET CONTROL SYSTEM62. on the role of surface orientation in relation to regression rates63. The Effect of Magnetic Field on The Performance of The Ion Thruster Discharge Chamber