All Stories

  1. An experimental-numerical approach to inferring gas-surface accommodation for vacuum chamber modeling
  2. Performance and discharge oscillation of a 1.5-kW-class double-channel Hall thruster with anode layer
  3. Effect of a Backward-Facing Step on Drag of a VLEO Satellite
  4. Facility pressure effects on thrust measurement of micronozzles and thrust correction for space applications
  5. Combustion Propagation on a Magnesium Wire in Water Vapor for Micropropulsion
  6. Study on Electrodes Design for MPD Thruster Using Water Propellant
  7. Facility Pressure Effects on Thrust Measurement of Micronozzles And its Correction for Space Applications
  8. Microwave Discharge Ignition of Metalized Fuel for Hybrid Rockets
  9. Performance Improvement by Vortex Combustion for a Magnesium-Loaded HTPB/N2O Hybrid Rocket for Small Spacecraft
  10. Rarefied Gas Simulation in Vacuum Chambers for Gas-Jet Propulsion: Toward Realizing a Numerical Vacuum Chamber
  11. Numerical Study of Facility Pressure Effects on Micronozzles for Space Propulsion
  12. Temperature measurement on condensed combustion products of magnesium with oxygen and water vapor
  13. Modeling of Ion Thruster Plume Neutralization Using Kinetic Simulations
  14. Experimental Study on Combustion of Water Vapor and Aluminum Powder for Chemical Micropropulsion
  15. Kinetic simulation of ion thruster plume neutralization in a vacuum chamber
  16. Three-Dimensional Kinetic Simulations of Carbon Backsputtering in Vacuum Chambers from Ion Thruster Plumes
  17. Fully Kinetic PIC Simulations of the Electrical Facility Effect on the Gridded Ion Thruster Testing
  18. Numerical Investigation of Carbon Sputtering and Transport for the Ion Thruster Testing in the Ground Facility
  19. Background Pressure Effect on Thrust Efficiency of Low-Reynolds-Number Nozzles
  20. Carbon Sputtering and Transportation in a Ground Facility during Electric Propulsion Testing
  21. Combustion of Magnesium Wires with Oxygen and Water Vapor
  22. Low-pressure-vaporization of water droplets on wall under normal and microgravity conditions
  23. Experimental Characterization of Nozzle Performance at Low Reynolds Numbers for Water Microthrusters
  24. The Measurement of 2-D Density Distribution at the Downstream of a Micronozzle of a Spacecraft Using Electron Beam Induced Fluorescence
  25. Feasibility Study of a Hybrid Thruster using Wire-Shaped Magnesium and Water for Application to Small Spacecraft
  26. Power Management of Lunar CubeSat Mission EQUULEUS Under Uncertainties of Power Generation and Consumption
  27. Experimental Study on Bulk Metal-Water Combustion for Small Spacecraft Propulsion
  28. Direct measurement of 1-mN-class thrust and 100-s-class specific impulse for a CubeSat propulsion system
  29. Mission to Earth–Moon Lagrange Point by a 6U CubeSat: EQUULEUS
  30. Flight Model Development and Ground Demonstration of Water Resistojet Propulsion System for CubeSats
  31. Assessment of Micropropulsion System Unifying Water Ion Thrusters and Water Resistojet Thrusters
  32. Experimental Characterization of Nozzle Performance at Low Reynolds Numbers for Water Resistojet Thrusters
  33. Comparison of Performance by different operation method of a Water Resistojet Propulsion System : AQUARIUS Installed on 6U CubeSat : EQUULEUS.
  34. Experimental Effects of Ambient Pressure on Nozzle Efficiency at Low Reynolds Numbers
  35. Fundamental Ground Experiment of a Water Resistojet Propulsion System: AQUARIUS Installed on a 6U CubeSat: EQUULEUS