All Stories

  1. Effect of a Backward-Facing Step on Drag of a VLEO Satellite
  2. Facility pressure effects on thrust measurement of micronozzles and thrust correction for space applications
  3. Combustion Propagation on a Magnesium Wire in Water Vapor for Micropropulsion
  4. Study on Electrodes Design for MPD Thruster Using Water Propellant
  5. Numerical Study of Facility Pressure Effects on Micronozzles for Space Propulsion
  6. Temperature measurement on condensed combustion products of magnesium with oxygen and water vapor
  7. Modeling of Ion Thruster Plume Neutralization Using Kinetic Simulations
  8. Experimental Study on Combustion of Water Vapor and Aluminum Powder for Chemical Micropropulsion
  9. Kinetic simulation of ion thruster plume neutralization in a vacuum chamber
  10. Three-Dimensional Kinetic Simulations of Carbon Backsputtering in Vacuum Chambers from Ion Thruster Plumes
  11. Numerical Investigation of Carbon Sputtering and Transport for the Ion Thruster Testing in the Ground Facility
  12. Background Pressure Effect on Thrust Efficiency of Low-Reynolds-Number Nozzles
  13. Carbon Sputtering and Transportation in a Ground Facility during Electric Propulsion Testing
  14. Combustion of Magnesium Wires with Oxygen and Water Vapor
  15. Low-pressure-vaporization of water droplets on wall under normal and microgravity conditions
  16. Experimental Characterization of Nozzle Performance at Low Reynolds Numbers for Water Microthrusters
  17. The Measurement of 2-D Density Distribution at the Downstream of a Micronozzle of a Spacecraft Using Electron Beam Induced Fluorescence
  18. Feasibility Study of a Hybrid Thruster using Wire-Shaped Magnesium and Water for Application to Small Spacecraft
  19. Power Management of Lunar CubeSat Mission EQUULEUS Under Uncertainties of Power Generation and Consumption
  20. Experimental Study on Bulk Metal-Water Combustion for Small Spacecraft Propulsion
  21. Direct measurement of 1-mN-class thrust and 100-s-class specific impulse for a CubeSat propulsion system
  22. Mission to Earth–Moon Lagrange Point by a 6U CubeSat: EQUULEUS
  23. Flight Model Development and Ground Demonstration of Water Resistojet Propulsion System for CubeSats
  24. Assessment of Micropropulsion System Unifying Water Ion Thrusters and Water Resistojet Thrusters
  25. Experimental Characterization of Nozzle Performance at Low Reynolds Numbers for Water Resistojet Thrusters
  26. Comparison of Performance by different operation method of a Water Resistojet Propulsion System : AQUARIUS Installed on 6U CubeSat : EQUULEUS.
  27. Experimental Effects of Ambient Pressure on Nozzle Efficiency at Low Reynolds Numbers
  28. Fundamental Ground Experiment of a Water Resistojet Propulsion System: AQUARIUS Installed on a 6U CubeSat: EQUULEUS