rootbrowseIAC-13C2session PP. Poster SessionPapers1. a new servo mechanism named eccentuator2. STUDY ON PHASED ARRAY ULTRASONIC NONDUSTRUCTIVE TESTING FOR ALUMINIUM ALLOY FRICTION STIR WELDING3. The Influence of Pre-oxidation on the Properties of PAN Based Carbon Fiber4. A New Method for CG Measurement in Determination of Mass Properties of Spacecrafts and Their Components5. design and examination of stage-separation connecting appliances of a missile6. water medium Hydraulic test methods for large liquid hydrogen tank7. A new reliability evaluation method of solar array unfolding mechanics based on test data on ground and on-orbit flight data8. Research on The Detail Design of Aircraft Wings9. Analysis of Coilable Lattice Mast10. Application of Non-Probabilistic Statistical Energy Analysis in Spacecraft’s vibro-acoustic Environment Prediction11. Global Damping Configuration of Large Space Truss Structure Based on Energy Finite Element Analysis12. effects of the high-temperature loading on the structure dynamic behavior13. Operational modal analysis of in-flight space launch vehicles on use of transmissibility measurements14. trajectory and deformation coupling calculation model for plane motion of a slender body15. constrained damping layer for dynamic loading attenuation of liquid rocket engine frame16. Observer-based two time control of free-flying flexible space manipulator17. resonant fixture design and test verification on shaker srs test18. Vibration Suppression of Space Structures Using Control Moment Gyroscopes as Actuators19. Analitical and Experimental Quantification of Stiffness and Damping for Dry Friction Dampers and Their Application to Impact.20. Modeling and simulation of a micro-vibration attenuating system based on flexible satellite model21. Nonlinear Vibration of a Bolt jointed Beam under Microslip22. Temperature Simulation Test of MTPS in Arc Tunnel23. Investigation on the design formulas for the nozzle flexible joint24. The effect of pore structure on strength and thermal conductivity of porous ZrO2 ceramics25. RESEARCH ON INFLUENCE OF PREFORM PARAMETERS ON PROPERTIES OF CARBON/CARBON COMPOSITES26. Mechanical Properties Test of 2D C/C Composites27. Fiber Content effect on the performance of Carbon /Carbon composites28. Heat treatment temperature effect on the thermal-physical properties of Carbon/Carbon composites29. Fibrous ceramic tiles for ultrahigh temperature thermal insulation30. Advanced MoSi2/NbSi2/Nb5Si3 multilayer coating on niobium alloy for the bipropellant rocket engine31. Thermal structure analysis of nozzle throat to braided C/C composite32. Study on EPDM insulation reinforced by PAA resin with excellent ablation and particles erosion resistance33. the anisotropy of thermal conductivity in diborides of zirconium and hafnium34. molding of low-cost composite ceramic insulation materials and its application in thermal protection of missile over large area35. RESEARCH ON ANTI-OXIDATION OF C/C COMPOSITES PREPARED BY SILICON CONTAINING POLYARYLACETYLENES36. effect of pyrolytic carbon interface on performance of c/c composite37. Boundary condition on stress calculation of the nozzle fixed case38. study on on-orbit micro-vibration monitoring and adaptive control system39. special fiber sensor for spacecraft application40. optimized thermal design of the gamma ray burst detector41. The Arc-heated Direct-Connected Testing Technology of Scramjet Combustor Thermal Protection System42. Development of Environment Simulator GVU-600 for Russian ISS-Reshetnev43. evaluation of prediction of InGaP2/GaAs/Ge solar cell performance in space radiation environment44. the study of atomic oxygen environment protection design and experiment techniques for spacecraft45. An equipment for collecting quantitative harmful gases in the spacecraft cabin46. delamination growth behavior in laminated composites under compressive fatigue loads47. Empirical evaluation of thermal contact resistance of bolted joint configurations employed in satellite applications fitted with interface materials under vacuum conditions48. dsmc modeling of rarefied aerodynamic features for lunar exploration re-entry vehicle49. Effect of a multi-disk aerospike on the aerothermodynamics of a reentry configuration50. A POSSIBLE FUTURE NEED OF AN ENFORCED THERMAL CONTROL OF THE EARTH51. Research on The Aerodynamic Heating Feature of Plane-Symmetric Aircraft52. MOLECULAR DYNAMIC SIMULATION OF COMPONENT AND PLATE INTERFACES IN A NANOSATELLITE53. Vibration signals analysis for solid lubrication of rolling ball bearings54. a new method to evaluate the damage extent of c/c composite material structure using acoustic emission technology55. Minimum-Mass Heat Shield for a Neptune Aerocapture Mission56. Research of bacterial antifungal decorative board used in space manned cabin57. Study on Ultra-temperature, High Heat Flux, Nonlinearity Aerodynamic Heating Environment Simulation and Thermo-machanical Testing Technique58. A New Concept of Three-dimensional Full Five-directional Braided Composites59. Potential applications of hybrid forming of aluminum alloys in aircrafts60. New weld filler wire and method of restraint intensity decrease characterization for Al-Li alloy 219561. research on composite high-pressure vessel technology applicable for space system62. PRELIMINARY INVESTIGATION OF AN INNOVATIVE SHAPE DEFORMABLE SPACE ROVER USING DIELECTRIC ELASTOMER ACTUATORS63. Preliminary Study on Laser Beam Weldability of Direct Laser Fabricated GH4169 for Aerospace Applications64. preparation and performance research of anti-electrostatic white thermal-control coatings for spacecrafts65. Analysis and prevention of cracking of carbonsteel components of aerospace product