Add to ORKGThe research for determining the space shuttle aerothermal environment is reported. Brief summaries of the low Reynolds number windward side heating test, and the base and leeward heating and high Reynolds number heating test are included. Also discussed are streamline divergence and the resulting effect on aerodynamic heating, and a thermal analyzer program that is used in the Thermal Environment Optimization Program
The aerothermodynamic performance of the Space Shuttle Orbiter during reentry is assessed from the c...
Results of wind tunnel heat transfer tests of 0.0175-scale Rockwell International Space Shuttle Vehi...
The initial research effort was an in-depth analysis of the shuttle main engine plumes in an effort ...
The Space Shuttle orbiter's thermal protection system (TPS), designed mainly on the basis of wind tu...
Heating rate and pressure measurements were obtained on a 25-O space shuttle model in a vacuum chamb...
The results are reported of research to provide thermal support in the design of the thermal protect...
A structural performance and resizing finite element thermal analysis computer program was used in t...
Quantitative estimates of the uncertainty in predicting aerodynamic heating rates for a fully reusab...
Work performed in support of radiation and convective base heating predictions in developing the spa...
Aerothermodynamic development flight test data from the first orbital flight test of the Space Trans...
A broad base of thermocouple and phase change paint data was assembled and correlated to the nominal...
The objective was to verify the design thermal environments for the Space Shuttle External Tank. The...
Procedures and methods for predicting aerothermodynamic heating to delta orbiter shuttle vehicles we...
A structural performance and resizing (SPAR) finite element thermal analysis computer program was us...
The experimental investigations performed on the NASA-Manned Spacecraft Center Space Shuttle orbiter...
The aerothermodynamic performance of the Space Shuttle Orbiter during reentry is assessed from the c...
Results of wind tunnel heat transfer tests of 0.0175-scale Rockwell International Space Shuttle Vehi...
The initial research effort was an in-depth analysis of the shuttle main engine plumes in an effort ...
The Space Shuttle orbiter's thermal protection system (TPS), designed mainly on the basis of wind tu...
Heating rate and pressure measurements were obtained on a 25-O space shuttle model in a vacuum chamb...
The results are reported of research to provide thermal support in the design of the thermal protect...
A structural performance and resizing finite element thermal analysis computer program was used in t...
Quantitative estimates of the uncertainty in predicting aerodynamic heating rates for a fully reusab...
Work performed in support of radiation and convective base heating predictions in developing the spa...
Aerothermodynamic development flight test data from the first orbital flight test of the Space Trans...
A broad base of thermocouple and phase change paint data was assembled and correlated to the nominal...
The objective was to verify the design thermal environments for the Space Shuttle External Tank. The...
Procedures and methods for predicting aerothermodynamic heating to delta orbiter shuttle vehicles we...
A structural performance and resizing (SPAR) finite element thermal analysis computer program was us...
The experimental investigations performed on the NASA-Manned Spacecraft Center Space Shuttle orbiter...
The aerothermodynamic performance of the Space Shuttle Orbiter during reentry is assessed from the c...
Results of wind tunnel heat transfer tests of 0.0175-scale Rockwell International Space Shuttle Vehi...
The initial research effort was an in-depth analysis of the shuttle main engine plumes in an effort ...