All Stories

  1. Design and Operation of a Calorimeter for Advanced Multilayer Insulation Testing
  2. Foreword
  3. Warm Pressurant Effects on Cryogenic Liquid Acquisition
  4. Warm Pressurant Gas Effects on the Static Bubble Point Pressure for Cryogenic LADs
  5. Inverted Outflow Ground Testing of Cryogenic Propellant Liquid Acquisition Devices
  6. Screen channel LAD bubble point tests in liquid hydrogen
  7. Warm Pressurization Gas Effects on the Liquid Hydrogen Bubble Point
  8. Mastering Cryogenic Propellants
  9. POROUS SCREEN APPLIED IN LIQUID ACQUISITION DEVICE CHANNEL AND CFD SIMULATION OF FLOW IN THE CHANNEL
  10. Human Exploration using Real-Time Robotic Operations (HERRO) -Crew Telerobotic Control Vehicle (CTCV) Design
  11. Liquid Acquisition Strategies for Exploration Missions
  12. Feasibility of Scavenging Propellants from Lander Descent Stage to Supply Fuel Cells and Life Support
  13. Phase field modeling of liquid jets in low gravity
  14. Cryogenic fluid transfer for exploration
  15. Settling Strategies for Fluid Management of Spacecraft
  16. Cryogenic Technology Development for Exploration Missions
  17. Vented Tank Resupply Experiment: Flight Test Results
  18. The role of flight experiments in the development of cryogenic fluid management technologies
  19. Flight Development for Cryogenic Fluid Management in Support of Exploration Missions
  20. Low Gravity Issues of Deep Space Refueling
  21. Approaches to Validation of Models for Low Gravity Fluid Behavior
  22. Parametric Investigation of Liquid Jets in Low Gravity
  23. Screen Channel Liquid Acquisition Devices for Cryogenic Propellants
  24. Modeling the restraint of liquid jets by surface tension in microgravity
  25. Technologies for refueling spacecraft on-orbit
  26. Models for liquid impact onboard Sloshsat FLEVO
  27. Planned axial reorientation investigation on Sloshsat
  28. Liquid Motion Experiment flight test results
  29. Status and design concepts for the hydrogen on-orbit storage and supply experiment
  30. Vented Tank Resupply Experiment - Flight test results
  31. An experiment to demonstrate key cryogenic technologies for solar thermal rockets
  32. Comparison of Liquid Hydrogen no-Vent Fill Test Data with Analytic Models
  33. Ground testing for the no-vent fill of cryogenic tanks - Results of tests for a 71 cubic foot tank
  34. Comparing the results of an analytical model of the no-vent fill process with no-vent fill test results for a 4.96 cu m (175 cu ft) tank
  35. Pulsed thrust propellant reorientation - Concept and modeling
  36. Evaluation of supercritical cryogen storage and transfer systems forfuture NASA missions
  37. Modeling of impulsive propellant reorientation
  38. Cryogenic transfer options for exploration missions
  39. Review and test of chilldown methods for space-based cryogenic tanks
  40. Ground testing of the nonvented fill method of orbital propellant transfer - Results of initial test series
  41. Initial experimentation on the nonvented fill of a 0.14 cu m (5 cu ft) dewar with nitrogen and hydrogen
  42. Evaluation of supercritical cryogen storage and transfer systems forfuture NASA missions
  43. Modeling of impulsive propellant reorientation
  44. Thermodynamic modeling of the no-vent fill methodology for transferring cryogens in low gravity