IP. Interactive Presentations - IAF SPACE PROPULSION SYMPOSIUM

Papers

1. Aquasonic II – Hybrid Propulsion analysis for 3D-printed fuel grains

2. Conceptual design of a hybrid sounding rocket to reach a target altitude

5. Design of a High Thrust Short Duration Solid Motor for Crew Escape System

6. Design and Experimental Analysis of Hybrid Rocket Engine Additively Manufactured Complex Port Geometries

7. EFFECT OF PYROLYSIS AND OXIDATION OF N-DECANE ON THE HEAT AND MASS TRANSFER CHARACTERISTICS OF HYDROCARBON FUELED SUPERSONIC FILM COOLING

8. Control System of LE-9 Engine using Electric Drive Valves

9. High porosity open cell metal foam supported catalysts for decomposition of 98% hydrogen peroxide

10. Development of a Consistent Burn Rate Determination Methodology for Ballistic Evaluation Motor

11. An overview of electric propulsion activities of Shanghai Institute of Space Propulsion

12. Laser Ablation Propulsion Launch System (LAPLaS) as a basis for New Access-to-Space Paradigm.

13. Effect of Prestrain on Uniaxial Tensile Behavior of HTPB Composite Propellant

14. A simplified chemical reaction mechanism for two-component RP-3 kerosene surrogate fuel and its verification

15. Two-dimensional tomographic reconstruction in combustion flows using multiple absorption transitions

16. CFD design method for capacitive POGO suppressor devices

17. Experimental Investigation of Injectors Design and their Effects on 1kN Performance Hybrid Rocket Motor

18. Additive Manufacturing Technologies applied to Space Propulsion

19. Experimental Studies of the 150N HAN-based Monopropellant Attitude Control thruster

20. Experimental Evaluation of the effect of Swirl oxidizer injection and aluminum particle addition in N2O-paraffin wax based laboratory Hybrid Rocket Propulsion System

21. Numerical study of temperature field during composite case co-curing process

22. Design and fabrication of MEMS thrust measurement system for performance evaluation of MEMS thruster

23. Energy conversion in wall catalytic steam reforming of hydrocarbon fuel at supercritical pressures

24. Life Cycle Prediction Of A Liquid Propellant Rocket Engine Thrust Chamber Using Unified Chaboche Viscoplastic Model

25. The Zurqui Engine: The First Central American and Caribbean Liquid Rocket Engine

26. Gelled propellant rocket motor and gas generator technology in Germany - an overview -

27. LES of HTPB/O2 and HTPB/N2O hybrid rocket engines

28. ARCLIGHT - A low cost plug-and-play RIT electric propulsion system

29. Design, Analysis and Test of a Hybrid Rocket Engine with a Multi-port Nozzle

30. Cold Flow Simulation of Compound Swirling Oxidizer Injection for Hybrid Rocket Propulsion

31. Results of Field-Emission Cathode Operation on the H-II Transfer Vehicle

32. Convolutional neural network based combustion mode classification for condition monitoring in a supersonic combustor

33. Development of a 25kN Hybrid Rocket Engine for the Stratos III sounding rocket

34. Electric propulsion system based on the air-breathing radio-frequency ion thruster using the upper atmosphere gases as propellant

35. Status of Orion European Service Module Propulsion Subsystem Qualification Testing

36. effect of chevron-like injector outlet on vortex-driven combustion instability

37. acoustic analysis on sub-scaled gas generator

38. Student Designed Propulsion System for a Reusable Flight Vehicle

39. Development of an Electro Thermal CubeSat Pulsed Plasma Thruster

40. Research on Failure Criterion of High Energy Solid Propellant under Complex Stress State

41. Plume Analysis of ADN Green Propellant Thruster for Satellite Attitude Control

42. Experimental Investigations of Plume Characteristics of the HET-40 Hall Thruster by Langmuir Probe

43. Effect of Nozzle Geometry on Counterflow Jets for Drag Reduction of a High Speed Vehicle

44. 3D imaging of burning aluminum particles in solid propellant using digital inline holography

45. LOx/LH2 engine demo platform

46. Transient Model of API Injector Using EcoSimPro for Expander Bleed Engine Application

47. Parameters analysis of non-linear combustion instability base on the pulsed trigger T-burner technique

48. DEVELOPMENT AND TESTING OF AN ADDITIVE LAYERED MANUFACTURED NOZZLE FOR A COLD GAS MICRO THRUSTER

49. Radiographic Inspection and Analysis of Case Bonded Solid Rocket Motor Defects

50. development of the mems-based nozzle using drie of tapered hole technology for cube satellite

51. A new European approach for Electric Propulsion on Small Satellites: HiperLoc-EP

52. Prediction and Validation of the Catalytic Decomposition of Hydrogen Peroxide in Dual-Catalytic Bed

53. A NEW SEMI-ANALYTICAL MODEL FOR PRELIMINARY ESTIMATION OF ION NUMBER DENSITY IN ELECTRIC THRUSTER PLUME

54. Control of Exhaust Gas Flow in Cryogenic Storage Tank Adopting Thermodynamic Venting System Technology

55. modeling and simulation of steady-state characteristics of cryogenic rocket engine

56. Design concepts and numerical simulation on the solid propellant microthruster for cubesat

56. structural integrity analysis of srm grain at low temperature ignition