All Stories

  1. An Assessment of Turbulence Models for MSR Sample Retrieval Lander Aerothermal Design
  2. Aerothermal Analysis and Environment Predictions for the Mars Sample Retrieval Lander (SRL)
  3. Hayabusa2 SHARC Spectro-Radiometric Calibration and Analysis
  4. Simulations of Hayabusa2 Atmospheric Entry and Comparisons with Data from the Imaging Campaign
  5. Emission Spectroscopic Characterization of the NASA IHF Plenum Plasma
  6. Rough-Wall Turbulent Heat Transfer Experiments in Hypersonic Free Flight
  7. Spectroscopic Analysis of Nonequilibrium Excited State Chemistry in a NASA Arc Jet
  8. Blunt-Body Aerothermodynamic Database from High-Enthalpy Carbon-Dioxide Testing in an Expansion Tunnel
  9. On the development of a new nonequilibrium chemistry model for Mars entry
  10. Equilibrium Radiative Heating from 9.5 to 15.5  km/s for Earth Atmospheric Entry
  11. Blunt-Body Heating and Pressure Database from High-Enthalpy, CO2 Testing in an Expansion Tunnel
  12. Investigation of Performance Envelope for Phenolic Impregnated Carbon Ablator (PICA)
  13. Tree Based Trajectory Planning for Mars Aerocapture
  14. HIFiRE-1 Turbulent Shock Boundary Layer Interaction -Flight Data and Computations
  15. Arc Jet Facility Test Condition Predictions Using the ADSI Code
  16. Conformal Phenolic Impregnated Carbon Ablator Arcjet Testing, Ablation, and Thermal Response
  17. Uncertainty Analysis and Validation of Radiation Measurements for Earth Reentry
  18. Transition Experiments on Blunt Bodies with Distributed Roughness in Hypersonic Free Flight in Carbon Dioxide
  19. Arcjet Testing in Shear Environment for Mars Science Laboratory Thermal Protection System
  20. Time-varying entry heating profile replication with a rotating arc jet test article
  21. Radiation Transport Analysis of Emission Spectroscopic Measurements in the Plenum Region of the NASA IHF Arc Jet Facility
  22. Measurement and Characterization of Mid-wave Infrared Radiation in CO2 Shocks
  23. Aeroheating Uncertainties in Uranus and Saturn Entries by the Monte Carlo Method
  24. The Effects of Surface Roughness on Turbulent Heat Transfer Measured in Hypersonic Free Flight