IP. Interactive Presentations

Papers

1. space gates: repurposing the mini-magnetosphereic plasma propulsion system as a mass driver

2. Aerothermodynamic experiment and simulation of spatial effects in a divert thrust chamber in hypersonic flow

3. the micro thrust automatic measurement system of plasma thruster

4. Design and Structural Characteristics of Gas Gimbaling Apparatus in LOX/Kerosene Rocket Engine

5. Ground testing of low-thrust self-pressurized hybrid motor

6. quasi-direct numerical simulation on atomization and mixing characteristics of a pair of impinging jets

7. Feasibility Study on Non-Toxic Hypergolic Bipropellant Thruster using Hydrogen Peroxide as an Oxidizer

8. Gas-phase nuclear rocket engines and propulsive mass for them.

9. fundamental energy propulsion systems

10. numerical simulation of grain's dynamic regression process for n2o/htpb hybrid rocket motors

11. experimental simulation investigation of diaphragm rupture and washing for rocket engine in arc heated air flow

12. Improved method for PIV measurement on high temperature vitiated supersonic flow-field

13. Research on Discharge Plasma Characteristics of An Ablative Pulsed Plasma Thruster via Emission Spectrometry

14. Verification of The Venus Technological Mission Module

15. Pocket Rocket: A radio-frequency electrothermal plasma micro-thruster

16. Frequency Behavior of Liquid Fueled Ramjet with variable area nozzle

17. wall temperature prediction of regenerative cooled rocket engine based on a coupled heat transfer model

18. Solar Thermal Propulsion Review

19. Electro-Magnetic Vacuum Thrust Producers (EMVTP)

20. investigation of flow induced pressure difference during high altitude simulation

21. Numerical Study for Simulating Liquid Rocket Engine Exhaust Plume Using Multi-species Un-reacted Flow Model

22. parametric study and sensitivity analysis of hybrid rocket motors with double-tube configuration

23. design and performance evaluation of hydrogen peroxide oxidizer hybrid thruster for sounding rocket system

24. analysis of system damping effect on time-lag based combustion instability model

25. Analysis of a Magneto-hydro-dynamic (MHD) Oblique Detonation Wave Engine

26. LIP's electric propulsion developments for chinese satellite platform

27. propellant-less propulsion system using microwaves

28. Thermal Test on an Ion Thruster

29. Experimental Investigation of Influencing Factors for Reliable Startup and Steady Work of 20W Microwave Electromal Thruster under Realistic Space Conditions

30. Innovative space propulsion technology using vacuum arc thrusters

31. INTERSTELLAR MISSION TO BARNARD'S STAR USING ADVANCED NUCLEAR PROPULSION METHODS

32. Theoretical modeling of the combustion of gel fuel droplets

33. SPACE QUALIFICATIONS OF THE MEMS-BASED SOLID PROPELLANT THRUSTER ARRAY FOR ON-ORBIT VERIFICATION USING CUBE SATELLITE

34. Three gridded ion engines for future high power electric propulsion missions

35. a novel design of mems based micropropulsion system for a nanosatellite

36. Validation with CFD Simulations of a Simplified Model of a Hybrid Rocket Motor

37. experimental study of flow separation in a subscale parabolic contour nozzle

38. sliding mode control control for hypersonic flight vehicle with time delay estimation and compensation

39. development of a low power cylindrical hall thruster propulsion system for microsatellites

40. Performance and environmental test results of a novel electric propulsion technology for small satellites

41. "Low Power Hall Effect Thruster Activities at Sitael"

42. Improved Modeling of Electric Sail (E-sail) Force Generation

43. Development of Low Power Electric Propulsion System for Micro-Satellites

44. An Overview of Hollow Cathodes Activities at Sitael

45. Performance increase of liquid rocket motor through pump modification for higher injection pressure operation

46. "MEPS: Programme Overview and System Development Status"

47. Development of a kW-level plasma thruster in project SAPERE –STRONG

48. Microthruster development for trajectory correction on upper stages and satellites

49. towards green propulsion for next-generation rockets with han-based monopropellants

50. Central binary collision of power-law model gel propellant droplets: effects of n and K on maximum deformation

51. Development of a Moveable Sleeve Injector with a Fixed Pintle for a Throttleable Rocket Combustor

52. A simple design for ablative liquid-fed pulsed plasma thrusters for small satellites

53. Low Frequency Combustion Instability Characteristics of Polyethylene-N2O Based Hybrid Rocket Motor

54. design optimization of a RBCC ejector mode using entropy analysis

55. Propulsion System of the Lunar Lander built for Google Lunar X Prize

56. Solid rocket motor burn simulation considering complex 3D propellant grain geometries

57. Experimental insight into the effect of sound intensity on smoldering combustion