rootbrowseIAC-14C2session PP. Poster SessionPapers1. optimal wiring configuration of multiple piezoelectric transducers for ssdi vibration suppression2. Researches into the Mechanical Characteristics and Optimization of the Linkage of a Strap-on Launcher3. Optimization of the multiple payloads adapter structure configuration4. Internal Pressure Design of Hypersonic Reusable Space Vehicle5. Connection Structure Design of Hanging Cryogenic Liquid Propellants Tank of Space Vehicle6. structural optimization of nano-porous insulation materials7. solar sails: a comparative study between kapton hn and kapton b membranes8. A New Identification Method for Multi-DOF Dynamic Interface Forces9. plastic zone at the mixed mode crack tip in nickel-based single crystal plate based on a modified yield criterion10. the improved failure mode effects and criticality analysis method based on analytic hierarchy process11. a code validation on hypersonic shock/boundary layer interaction Flows over a hollow cylinder/flare configuration12. parameter optimization of the transition zone of large thin-walled tank structure13. The analysis of SH-waves propagation behaviors in periodic piezomagnetic-piezoelectric composite materials14. An assembly tolerance analysis and optimization method based on Monte Carlo Simulation15. The effects of stacking sequence of the skin and stiffener upon the delamination growth process for composite advanced grid stiffened structures (AGS)16. Microstructure analysis of three-dimensional full five-directional braided composites17. application of partial least squares regression method for mathematical modeling of rocket aerodynamic data18. optimal control for shape and vibration of space intelligent truss structure with piezoelectric actuators19. investigation of the aerodynamic characteristic during folded rudder deployment20. Thermal state of solar sail with strain-dependent optical parameters21. Integrative optimized design of highly reliable repetitive folding spatial mechanism and structure22. dynamic modeling of heat transfer in thermal-acoustic fatigue tests of hypersonic and re-entry vehicles23. dynamic singular modeling, robust fuzzy sliding control and flexible vibration active suppression for free-floating space robot with flexible joint and flexible manipulator24. Arc-heated Experimental Method Investigation on the Scramjet Combustor Wall Thermal Protection Material25. Testing of Combustor Chamber Material in Arc Jet Flow Mixing with Transverse Injected Water26. Thermal Analysis of a Satellite Borne Antenna27. analytic design of the phase change material for thermal control of the satellite component in periodic duty28. A new concept variable resistance radiator29. Thermal Modeling of CubeSat Standard NanoSatellites30. Equilibrium Molecular Dynamics Modeling of Diffussion and Adsorption of Fluids in Armchair Single Walled Carbon-nanotube31. DEVELOPMENT OF A THERMAL CONTROL SYSTEM FOR SOUTH AFRICA'S NEXT GENERATION EARTH OBSERVATION SATELLITE32. Arc-heating Test Simulation Method of Engine Thermal Barrier Coating (TBC) Materials with High-emissivity Rear Coating33. A Case Study on the Deployment Process for Inflatable Support Booms34. Design and optimization of variable density multilayer insulation for cryogenic tank35. Simulative and experimental study of plasma distribution of Electric Propulsion Thruster36. Design and Performance Evaluation of Reusable Launch Vehicle Aerodynamic Layout37. Optimization of stiffened shell structures with stability objective/constraint based on kriging surrogate model and the explicit FEM38. studies on aero thermodynamics performance in the gap between the base side and the baseboard of air rudders in arc wind tunnel39. Nanocomposites for EMI shielding: A Comparative Study of EMI Shielding Properties of Carbon fillers, and Multi-Walled Carbon Nanotube Filled Polymer Composites40. Observer-based augmented singular perturbation adaptive control of free-floating flexible space manipulator41. flexural wave scattering by a circular hole in rectangle thin plate42. Ink-jetted functional circuitry for heaters and strain-gauges aerospace applications43. Optimization of High Damping Composite Fixing Panel for Launch Vehicle Electronic Apparatus44. Pulsating heat pipe for thermal control of spacecraft electronics cooling: theoretical and experimental investigations45. analysis of large flexible spacecraft elastic vibration model and impact on attitude control system46. Graphene/DNA nanostructured films for bioinspired sensing of UV radiation effects47. The Control-Oriented Aerodynamic Design and Analysis for Hypersonic Waverider48. curvature control of membrane laminated film structure with sputtering49. investigation of fairing typical attitude aerodynamic characteristic during fairing separation50. Modeling and Analysis of Reinforced Membranes for Space Applications51. Structural performance and helium / hydrogen permeability rates of fused deposition modeling polymers at cryogenic temperatures52. ablative performance comparison study of lightweight and dense 3d carbon fabric composites53. the research of solar wing deployment support mechanism based on the tape spring54. Evaluation and Test of Polyamide Gears for Pointing Mechanisms55. analysis of boundary layer suppression in unsymmetrical airfoil using piezo electric effect56. identification of damaged configurations in a truss-type structure57. Accurate satellite mathematical model generation for line of sight jitter evaluation using semi-direct updating techniques with modal survey test58. triangle-section coilable mast development for buaa-sat59. A few varieties of measurement methods for testing composite structures60. the POGO stability analysis of large liquid rocket considering longitudinal, lateral and torsional mode in structural system61. spectral dependency of polarization properties for the lunar regolith62. Thermal Designing and Analysis Using ANSYS for ‘Pratham’ Student Satellite IIT Bombay63. Model-free control for active multi-mode vibration confinement of spaceborne truss using a six-degree-of-freedom Stewart platform64. New reinforcement method of impact bruising alloy thin-wall tank65. Preliminary Thermal and Orbital Spin Analysis of NanoSatellites66. Study on Prediction Method of Aerodynamic Characteristics Analysis for Mars Entry Capsules67. Integrated design proposal for a lightweight and efficient heat protection and insulation technology68. dynamics modeling and radial basis function neural network adaptive control of dual-arm flexible-joint space robot with parameter unknown69. INCREASED ZERO REACTION WORKSPACE OF A HYPER-REDUNDANT FREE-FLOATING SPACE ROBOT70. Biochemical detector based on the controlled tunneling between detector nanostructures and analyte71. heat transfer characteristic of confined jet array impingement cooling for high heat flux applications of spacecraft72. Study on large launch vehicle segmengts connected by bolts73. An Improved Test System for Thermal-Structural Test of Thin Shell Parts of Spacecraft.74. CEVHER - Vertical Take-Off Landing (VTOL) with Coanda Effect75. Capillary infiltration behavior of C/C-preforms for production of C/C-SiC composites via LSI76. High-precision temperature control method study based on hiberarchy thermal control77. research on passive orbital disconnect structs of cryogenic tank78. analysis and verification of satellite thermal deformation influence on positioning accuracy79. investigation of ablative properties of lightweight carbon/phenolic composites80. The synthesis and pyrolysis mechanism of resole phenolic resin for ablative materials81. Deployment Dynamics of a Large Deployable Mesh Antenna Considering Anti-entanglement Techniques