Science Objectives and Performance of a Radiometer and Window Design for Atmospheric Entry Experiments
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[1] R. Craig,et al. VUV shock layer radiation in an arc-jet wind tunnel experiment , 1994 .
[2] Imelda Terrazas-Salinas. Development of radiometer windows for atmospheric entry vehicles , 1993 .
[3] R. Craig,et al. Spectral measurements of shock layer radiation in an arc-jet wind tunnel , 1993 .
[4] L. Carlson. Approximations for hypervelocity nonequilibrium radiating, reacting,and conducting stagnation regions , 1988 .
[5] Elizabeth M. W. Pincha,et al. Effect of surface catalysis on heating to ceramic coated thermal protection systems for transatmospheric vehicles , 1988 .
[6] James N. Moss,et al. Nonequilibrium thermal radiation for an aeroassist flight experiment vehicle , 1988 .
[7] J. Arnold,et al. Radiometer experiment for the aeroassist flight experiment , 1985 .
[8] C. Park,et al. Radiation Enhancement by Nonequilibrium in Earth's Atmosphere , 1985 .
[9] Chul Park,et al. Problems of Rate Chemistry in the Flight Regimes of Aeroassisted Orbital Transfer Vehicles , 1984 .
[10] Brent Wedding,et al. Measurements of High‐Temperature Absorption Coefficients of Glasses , 1975 .
[11] Ellis E. Whiting,et al. PAET, an entry probe experiment in the earth's atmosphere. , 1973 .