IP. Interactive Presentations - IAF SPACE PROPULSION SYMPOSIUM

Papers

1. PEPE: A low cost, reliable, reusable, user- and environment- friend Propulsion System

2. Optimized orbit transfer of a Gravidyne with low-thrust propulsion

3. Experimental Investigation on Throttling Transient Response of Bipropellant Thruster Using Cavitating Venturi Valve.

5. Physical properties and ignition characteristics of hypergolic propellant with oxidizing additives

6. ignition delay and thermoacoustic coupling in hybrid rocket combustion

7. two-phase, multicomponent hydrogen peroxide blowdown injector modelling and tests comparisons

9. Numerical and experimental investigation of lambda type seals in high-pressure cryogenic bolted joints

10. Designing a nuclear electric propulsion system for future Pluto missions

11. ST-40 Hall Thruster Testing with LaB6 Hollow Cathode

12. Strategy for Simultaneous Hydrogen Trapping and Metallic Grain Size Control in Cermet Fuels for Nuclear Thermal Propulsion

13. Conceptual Design of a N2O/Paraffin Hybrid Sounding Rocket

14. Parametric design and testing of explosion-preventive solid propellant rocket engines in the event of unexpected behavior during combustion

15. Nuclear Thermal Propulsion for In-Space Applications focusing Beryllium as the Working Fluid and Graphite and FLiBe as Moderator and Coolant and Thorium Blanket

16. Propellant grain design for Solid strap-on Booster operating under Martian condition and selecting the appropriate propellant.

17. The Relativistic Mass Ratio in Ultrarelativistic Photon Rockets

19. Pulsed Plasma Thruster for Deep Space Exploration

20. Electrodeless plasma thruster concepts for high-power propulsion systems

21. Aerodynamic analysis on JAXA’s experimental vehicle for hypersonic flight

22. Dynamic Modeling and Simulation of a Hydrogen Peroxide Monopropellant Thruster

23. Three-Dimensional MHD Analysis of Magnetic Plasma Drag with Coils Placed on Three Axes

24. Conditions for the long-term existence of spacecraft with air-breathing electric propulsion in ultra-low orbits about planets

25. A Novel Design Usage of Thermoelectric Materials in Aerospike Engines

26. A Comparison Study on the Feasibility of Two Low Sloshing Configurations for Small Satellite Magnetic Fluid Actuation

27. The nano-probe by the photon transportation in the Deep Space

28. 9tonf staged combustion cycle liquid rocket engine startup analysis

29. Hypergolic ignition characterization of less-toxic bipropellants using Hydrocarbon fuel blend and Hydrogen Peroxide

30. Development Status of the SPS-40 Propulsion System

31. HYDROGEN-ENRICHED LIQUID METHANE AND LIQUID ETHANOL AS A TRANSITIONAL SOLUTION TOWARDS SUSTAINABILITY IN TERMS OF TECHNICAL FEASIBILITY FOR AEROSPACE MISSIONS

33. Development of Ultra High DN Ceramic Ball Bearing for Cryogenic Rocket Engine Turbopump

34. The effect of aerodynamic heating to cryogenic propellant discharge

35. preliminary screening of catalytic beds for hydrogen peroxide thrusters with thrust level lower than 0.5 N

36. Numerical Simulation of Flow Atomization caused by Two Impinging Liquid Jets

37. Rapid Design of a Small Scale KeroLOx Flight Vehicle Propulsion System

38. FEASIBILITY ANALYSIS FOR ELECTRIC PROPULSION SYSTEMS FOR SHORT TERM INTERPLANETARY MISSIONS

39. Design and development of Latching Solenoid valve for Active Pressure Regulation System

40. Computational model for performance prediction of a nitrous oxide / eicosane hybrid rocket engine

41. Common pitfalls of testing hybrid rocket engines at student led facilities

42. Vacuum Arc Thruster architecture for green orbit maintenance with small satellite missions

43. Experimental & Numerical Investigation of GOx/GCH4 Combustion in a 7-Element Rocket Combustor

44. Numerical study on n-decane heat transfer under supercritical pressure in regenerative cooling channel

45. Integrated internal and external ballistics for sounding rocket design

46. Numerical estimation of heat loss and thrust performance characteristics in micro propulsion

47. Comparative analysis of numerical models of film and regenerative cooling in thrust chamber at high pressure

48. multi-scale numerical study on atomization dynamics of gas-liquid pintle injector

49. Modeling of wall-bounded high pressure flows in Liquid Rocket Engines

50. High Flux Hybrid Motor Development with Distributed Tube Injector

51. Research on Acoustic Closed-End Device for Hydraulic Excitation Test of LRE

52. RESEARCH ON ELECTRIC SPACE PROPULSION AT ITALIAN AEROSPACE RESEARCH CENTRE: status and future enhancement

53. Effect of H2O2 concentration and catalytic ratio on the autoignition characteristics of RP-3 kerosene under catalytic ignition engine-like conditions

54. A Review: On the various FEEP thrusters present in the Industry and their Performance Comparison

55. Vacuum testing of 3D printed 1N Hydrogen Peroxide thruster and a novel platinum catalyst

56. Lessons learned during SRAD hybrid rocket motor development

57. Using differential pressure sensor to measure nitrous oxide level in a tank