rootbrowseIAC-17C4session IPIP. Interactive PresentationsPapers1. Spacecraft-plasma interactions of a cubesat equipped with miniaturized feep thrusters2. Advanced Propulsion Control System(APCS) Model using Intelligent Techniques3. Transient Responses of Turbulent Heat Transfer of N-Decane at Supercritical Pressure and Temperature below 800 K4. design, manufacture and testing of a 20 cm electron cyclotron resonance gridded ion thruster and neutraliser using additive manufacturing5. wavelet packet analysis of time-frequency characteristic of the LOX/Kerosene rocket engine due to heavy impact6. Application of Particle-In-Cell Simulation Techniques in the Analysis and Optimisation of Magnetic Nozzle Geometries7. Multi-objective Design Optimization of the Cusped Field Thruster for Micro-Satellite Platforms8. Study of Effect of Neutral Flow and Electron Transport in Wall Less Hall Thruster Concept9. Control of Miniaturized Electrospray Ion Thrusters for CubeSat Designs10. Coilgun Acceleration Model Containing Interactions Between Multiple Coils11. Overview of Electric Propulsion Developments at TU Dresden for Micro and Small-Satellites12. investigation of selective laser melting (slm) for production of microwave ion thruster accelerator grids13. Evaluation of Quasi-Steady Operation of MPD Thruster using Electric Double-Layer Capacitors14. Closed-loop Thrust Control for Micropropulsion Systems15. choi-williams ditribution analysis for fault detection of the liquid propellant rocket engine16. Numerical Simulation of Flow Characteristics in Methane Transverse Jet17. Two Dimensional Axisymmetric Navier-Stokes Analysis of Hybrid Rocket Intrinsic Instability18. Study of Ignition Transient in 2m Diameter Segmented SRM19. An additively-manufactured CNG/GOX aerospike rocket engine: Test results, performance and analysis20. Study on auto-ignited hybrid rocket based on n2o oxidizer using catalytic ignition system21. Early Studies and Fire Tests of a Green Liquid Apogee Engine Based on Decomposition of 98% Hydrogen Peroxide22. Applications for 3D printing in the Design of Hall Effect Thrusters23. Effect of Prestrain on Dynamic Mechanical Properties of HTPB propellant24. numerical investigation on detonation process of pulse detonation engine with hypergolic propellants25. investigation of catalytic re-ignition process in hydrogen peroxide hybrid rocket motors26. numerical simulation of catalytic decomposition and combustion process in an hydroxylammonium nitrate (han)-based monopropellant thruster27. Assessment of combustion instability mechanisms based on an energy balance analysis28. Investigation on the Near-nozzle Field Flow of Liquid Jet in a Supersonic Crossflow29. A Theoretical Study on Throttle Ranges of O/F Controllable Hybrid Rocket Propulsion Systems30. Numerical simulation of the start process of a han-based mono-propellant rocket thruster31. Systematic performance analysis of cubesat propulsion systems using the high performance satellite dynamics simulator HPS32. Development of 2,500 N class hydrogen peroxide/polyethylene hybrid rocket for lab-scale sounding rocket application33. Numerical Simulation of Influence of Injector Parameters on Combustion in LOX/Methane Engine34. Material Compatibility of Six Metal Alloys with HAN based Green Monopropellant Fuel Blend35. particle damping characteristics of low and medium frequency oscillation in solid rocket motor36. Feasibility of FDM Ablative Ceramic Materials for Low-Cost Propulsive Systems37. Optimization of catalytic bed geometry for 98% hydrogen peroxide monopropellant thruster38. Shallow Water Tests of Seconary Injection Thrust Vector Control of Aerospike Nozzles39. Numerical and experimental study of supersonic film cooling with cracking hydrocarbon fuel as coolant40. Design and Experimental Characterization of a Hydrogen Peroxide-Ethanol based Combustor for Space Propulsion42. Primary In-Space Experimental results of the HEP-100MF Electrical Propulsion System43. Reusable TSTO Conceptual Vehicle Designs using the TRRE Engine44. Turbine reheater: a new paradigm for hypersonic flight propulsion45. LES of Streamwise Vortex on Supersonic Mixing employing Hypermixer46. Experimental and Computational Studies of Supersonic Combustion Characteristics of HyperMixer in Mach 8 Flight Condition47. Preliminary studies on physical definition and discrimination of rocket-ejector mode of RBCC Engine48. The preliminary study of severity level of structural discontinuities in paraffin grain of hybrid propellant rocket49. Analysis of cavitation characteristics of pumps used in liquid rocket engines by using multihole orifice plate50. On the Electrical Propulsion of a Solar Sail51. Physical grounds and control optimization of ultralow-orbit spacecraft with electric ramjet