P. Poster Session

Papers

1. The Research on the Principle of EMdrive Propulsion Technology

2. LOX-kerosene liquid rocket engine with a thrust of 9.8 MN

3. Start-up Transient Simulation of 60t Class LOX/Methane Liquid Rocket Engine

4. Numerical Simulation for the Satellite Propulsion System

5. The comparison of combustion characteristics between oxygen/methane and oxygen/propane for bipropellant thruster

6. characterisation and electrolytic decomposition of adn-han mixture in a polymer micropropulsion system

7. the influence of nitrogen pressurization of liquid oxygen quality

8. cfd modeling activities on testing technology of liquid rocket engine

9. Oxygen and methane liquid propellant rocket engines for reusable space transport system

10. ANALYTICAL STUDY RESULTS OF GREEN PROPELLANT APPLICATION POSSIBILITY IN LANDING MODULE AND SPACE TUG ENGINES

11. Developing Tendency in Liquid Rocket Engine Research and Corresponding Key Technologies

12. The service life assessment of NEPE propellant

13. Mechanical behavior research for air-ground inconsistency of solid rocket motor

14. solid rocket motor segment dismantling, cause analysis and reassembly

15. ultrasonic measurement of solid fuel regression rate of a hybrid slab motor

16. Design and performance evaluation of lab-scale hybrid thruster using catalytically decomposed hydrogen peroxide oxidizer

17. Numerical Simulation and Testing of H2O2 - LDPE Hybrid Rocket Motor with Diaphragm

18. Experimental Investigation on Combustion of Aluminum in the AP/HTPB Composite Propllent

19. Transient Simulation of Operation Process in a Throttleable Hybrid Rocket Motor

20. biglobal instability of compressible taylor-culick flow

21. The comparison of the different models of the burning regression rate in the hybrid rocket motor

22. Replacement of hydrazine-based systems by means of hybrid rockets

23. experimental investigation of fuel regression rate in HTPB based lab-scale hybrid rocket motor

24. The Numerical Simulation of a Staged Transverse Injection Behind a Rearward Facing Step Into a Mach 2 Stream in a Confined Environment and its application in the development of scramjet technology

25. Design and simulation of gas oxygen / methane vortex cooling thrust chamber

26. Viscoplastic and elasto-plastic thermal-structure analysis of the reusable rocket thrust chamber

27. The TVC Systems for a Chinese Liquid Oxygen and Kerosene Launch Vehicle

28. Heat Exchange and Pressure Drop induced by Sloshing

29. Research on the scheme and hot fire tests of combustion devices for 100kN LOX/methane rocket engine

30. development of fluid control components for liquid propulsion systems of isro

31. Research of laser ignition of propellant oxygen-kerosene in the model set

32. Effects of electrode geometry on magnetic field distribution in a pulsed plasma thruster

33. Development of Scaling Models for Applied Field Magnetoplasmadynamic Thrusters

34. evaluation of the performances of a helicon plasma thruster

35. Study on the Plume characteristics of Pulsed Plasma Thruster

36. Development of a Charge Exchange Thruster for Nanosatellite Missions

37. Design, manufacturing and characterization of a 1 milliNewton class FEEP emitter

38. Thermionic emission by a thin bare tether with low-W coating

39. DEVELOPMENT AND TESTING OF THE INERTIAL ELECTROSTATIC CONFINEMENT DIFFUSION THRUSTER

40. Experimental investigation of self-excitation influence on low frequency oscillations of SPT

41. Experimental optimization of preheating duration in low-power resistojet

42. Fabrication of self-ordered nano-scale emitters in FEEP

43. study of density jump phenomenon under the effect of circuit loss in a helicon plasma thruster

44. The Dynamic Operation of a High Q EmDrive Microwave Thruster

45. Study on the operation process of pulsed plasma thrusters by a modified electromechanical model

46. The limiting current of the ion beam in laboratory operating conditions of the Hall thruster

47. Interdependence between integral characteristics of Hall thrusters

48. Integration Considerations in Satellite Propulsion Systems: Hall Thrusters versus Ion Engines

49. Study and Analysis of Plume Backflow From a Lithium Magnetoplasmadynamic Thruster Enabled on an Experimental Nano-Satellite

50. MAGNETOPLASMADYNAMIC ELECTRIC PROPULSION THRUSTER BEHAVIOR AT THE 27 MEGAWATT LEVEL – ISRO Sponsored Project

51. Effects of electrode configuration on ablative pulsed plasma thruster performance

52. investigation on wave structure and power deposition in a helicon plasma thruster

53. Chemical structral and distribution characteristics of the Pulsed Plasma Thruster plume depostion

54. INITIAL FLIGHT TEST RESULTS OF THE LIPS-200 ELECTRIC PROPULSION SYSTEM ON SJ-9A SATELLITE

55. New thrust measurement device for 10N rocket engine

56. multiscale simulations of primary atomization for two impinging jets

57. Oxidizer-Rich Preburner-Feed System Medium Frequency Coupled Stability Investigation

58. Flow-induced Vibrations of Liquid Rocket Engine Bellows Subjected to Internal High Pressure and Velocity

59. the effect of ring with large eddy simulation in the flow development cylindrical duct

60. Investigation of Shutdown Dynamic Characteristics for LOX/Kerosene Rocket Engine

61. Microhybrid engine numerical and experimental results

62. space propulsion system using earths magnetic field

63. The isotope Stirling power system energy management

64. Fusion-Fission Hybrid Pulsed Propulsion System for Improved Space Transportation

65. theoretical analyses of performance of the integrated rocket-ramjet engine

66. Investigation of Ramjet Engine Real-time Simulator Modeling and Simulating

67. wind tunnel research on forward-facing cavity flow

68. Summary and Development in Research on High-energy Laser Propulsion

69. experimental study of boron ignition and combustion in convective flow

70. Analysis of Heat Release Distribution in Scramjet Combustor Using Wall Pressure Based One Dimensional Model

71. Experimental Investigation and Numerical Simulation on Combustion Characteristic of Solid Fuel Ramjet

72. Numerical Investigation of a Ma 10 Stream Traced Scramjet at Off Design Conditions

73. Analysis of a combined multi-mode detonation wave engine for aerospace craft

74. A New Hybrid-Rocket-Based Combined-Cycle Propulsion System Concept