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  • IP. Interactive Presentations

    Papers

    1. Spacecraft-plasma interactions of a cubesat equipped with miniaturized feep thrusters

    2. Advanced Propulsion Control System(APCS) Model using Intelligent Techniques

    3. Transient Responses of Turbulent Heat Transfer of N-Decane at Supercritical Pressure and Temperature below 800 K

    4. design, manufacture and testing of a 20 cm electron cyclotron resonance gridded ion thruster and neutraliser using additive manufacturing

    5. wavelet packet analysis of time-frequency characteristic of the LOX/Kerosene rocket engine due to heavy impact

    6. Application of Particle-In-Cell Simulation Techniques in the Analysis and Optimisation of Magnetic Nozzle Geometries

    7. Multi-objective Design Optimization of the Cusped Field Thruster for Micro-Satellite Platforms

    8. Study of Effect of Neutral Flow and Electron Transport in Wall Less Hall Thruster Concept

    9. Control of Miniaturized Electrospray Ion Thrusters for CubeSat Designs

    10. Coilgun Acceleration Model Containing Interactions Between Multiple Coils

    11. Overview of Electric Propulsion Developments at TU Dresden for Micro and Small-Satellites

    12. investigation of selective laser melting (slm) for production of microwave ion thruster accelerator grids

    13. Evaluation of Quasi-Steady Operation of MPD Thruster using Electric Double-Layer Capacitors

    14. Closed-loop Thrust Control for Micropropulsion Systems

    15. choi-williams ditribution analysis for fault detection of the liquid propellant rocket engine

    16. Numerical Simulation of Flow Characteristics in Methane Transverse Jet

    17. Two Dimensional Axisymmetric Navier-Stokes Analysis of Hybrid Rocket Intrinsic Instability

    18. Study of Ignition Transient in 2m Diameter Segmented SRM

    19. An additively-manufactured CNG/GOX aerospike rocket engine: Test results, performance and analysis

    20. Study on auto-ignited hybrid rocket based on n2o oxidizer using catalytic ignition system

    21. Early Studies and Fire Tests of a Green Liquid Apogee Engine Based on Decomposition of 98% Hydrogen Peroxide

    22. Applications for 3D printing in the Design of Hall Effect Thrusters

    23. Effect of Prestrain on Dynamic Mechanical Properties of HTPB propellant

    24. numerical investigation on detonation process of pulse detonation engine with hypergolic propellants

    25. investigation of catalytic re-ignition process in hydrogen peroxide hybrid rocket motors

    26. numerical simulation of catalytic decomposition and combustion process in an hydroxylammonium nitrate (han)-based monopropellant thruster

    27. Assessment of combustion instability mechanisms based on an energy balance analysis

    28. Investigation on the Near-nozzle Field Flow of Liquid Jet in a Supersonic Crossflow

    29. A Theoretical Study on Throttle Ranges of O/F Controllable Hybrid Rocket Propulsion Systems

    30. Numerical simulation of the start process of a han-based mono-propellant rocket thruster

    31. Systematic performance analysis of cubesat propulsion systems using the high performance satellite dynamics simulator HPS

    32. Development of 2,500 N class hydrogen peroxide/polyethylene hybrid rocket for lab-scale sounding rocket application

    33. Numerical Simulation of Influence of Injector Parameters on Combustion in LOX/Methane Engine

    34. Material Compatibility of Six Metal Alloys with HAN based Green Monopropellant Fuel Blend

    35. particle damping characteristics of low and medium frequency oscillation in solid rocket motor

    36. Feasibility of FDM Ablative Ceramic Materials for Low-Cost Propulsive Systems

    37. Optimization of catalytic bed geometry for 98% hydrogen peroxide monopropellant thruster

    38. Shallow Water Tests of Seconary Injection Thrust Vector Control of Aerospike Nozzles

    39. Numerical and experimental study of supersonic film cooling with cracking hydrocarbon fuel as coolant

    40. Design and Experimental Characterization of a Hydrogen Peroxide-Ethanol based Combustor for Space Propulsion

    42. Primary In-Space Experimental results of the HEP-100MF Electrical Propulsion System

    43. Reusable TSTO Conceptual Vehicle Designs using the TRRE Engine

    44. Turbine reheater: a new paradigm for hypersonic flight propulsion

    45. LES of Streamwise Vortex on Supersonic Mixing employing Hypermixer

    46. Experimental and Computational Studies of Supersonic Combustion Characteristics of HyperMixer in Mach 8 Flight Condition

    47. Preliminary studies on physical definition and discrimination of rocket-ejector mode of RBCC Engine

    48. The preliminary study of severity level of structural discontinuities in paraffin grain of hybrid propellant rocket

    49. Analysis of cavitation characteristics of pumps used in liquid rocket engines by using multihole orifice plate

    50. On the Electrical Propulsion of a Solar Sail

    51. Physical grounds and control optimization of ultralow-orbit spacecraft with electric ramjet