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  • 1
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    Time-varying Entry Heating Profile Replication with a Rotating Arc Jet Test Article (2014)
    In:  CASI
    Details
    Publication Date: 2019-07-13
    Description: A new approach for arc jet testing of thermal protection materials at conditions approximating the time-varying conditions of atmospheric entry was developed and demonstrated. The approach relies upon the spatial variation of heat flux and pressure over a cylindrical test model. By slowly rotating a cylindrical arc jet test model during exposure to an arc jet stream, each point on the test model will experience constantly changing applied heat flux. The predicted temporal profile of heat flux at a point on a vehicle can be replicated by rotating the cylinder at a prescribed speed and direction. An electromechanical test model mechanism was designed, built, and operated during an arc jet test to demonstrate the technique.
    Keywords: Ground Support Systems and Facilities (Space)
    Type: ARC-E-DAA-TN11922 , AIAA Aviation 2014; Jun 16, 2014 - Jun 20, 2014; Atlanta, GA; United States|AIAA/ASME Joint Thermophysics and Heat Transfer Conference; Jun 16, 2014 - Jun 20, 2014; Atlanta, GA; United States
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 2
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    Flow Property Measurement Using Laser-Induced Fluorescence in the NASA Ames Interaction Heating Facility (2011)
    In:  CASI
    Details
    Publication Date: 2019-07-13
    Description: The spectroscopic diagnostic technique of two photon absorption laser-induced fluorescence (TALIF) of atomic species has been applied to single-point measurements of velocity and static temperature in the NASA Ames Interaction Heating Facility (IHF) arc jet. Excitation spectra of atomic oxygen and nitrogen were recorded while scanning a tunable dye laser over the absorption feature. Thirty excitation spectra were acquired during 8 arc jet runs at two facility operating conditions; the number of scans per run varied between 2 and 6. Curve fits to the spectra were analyzed to recover their Doppler shifts and widths, from which the flow velocities and static temperatures, respectively, were determined. An increase in the number of independent flow property pairs from each as-measured scan was obtained by extracting multiple lower-resolution scans. The larger population sample size enabled the mean property values and their uncertainties for each run to be characterized with greater confidence. The average plus or minus 2 sigma uncertainties in the mean velocities and temperatures for all 8 runs were plus or minus 1.4% and plus or minus 11%, respectively.
    Keywords: Fluid Mechanics and Thermodynamics
    Type: ARC-E-DAA-TN2704 , 49th Aerospace Sciences Meeting and Exhibit; Jan 04, 2011 - Jan 07, 2011; Orlando, FL; United States
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 3
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    Shock Layer Radiation Measurements and Analysis for Mars Entry (2009)
    In:  CASI
    Details
    Publication Date: 2019-07-13
    Description: NASA's In-Space Propulsion program is supporting the development of shock radiation transport models for aerocapture missions to Mars. A comprehensive test series in the NASA Antes Electric Arc Shock Tube facility at a representative flight condition was recently completed. The facility optical instrumentation enabled spectral measurements of shocked gas radiation from the vacuum ultraviolet to the near infrared. The instrumentation captured the nonequilibrium post-shock excitation and relaxation dynamics of dispersed spectral features. A description of the shock tube facility, optical instrumentation, and examples of the test data are presented. Comparisons of measured spectra with model predictions are also made.
    Keywords: Space Radiation
    Type: ARC-E-DAA-TN315 , 3rd International Workshop on Radiation of High Temperature Gases in Atmospheric Entry; Sep 30, 2008 - Oct 03, 2008; Heraklion; Greece
    Format: application/pdf
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    NASA TECHNICAL REPORTS
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