Entry heating flight data and wind tunnel data on the lower windward and upper lee side centerline, lower wing 50% and 80% semi-spans, side fuselage and payload bay door, Z-400 and 440 trace aft of X/L=0.2, and OMS Pod trace 3, are presented for the first five flights of the space shuttle orbiter. Heating rate distributions are presented in terms of normalized shock Reynolds number to show the sensitivity of heating to these parameters. The surface heating rates and temperatures were obtained via the JSC NONLIN/INVERSE computer program
A structural performance and resizing (SPAR) finite-element computer program and NASA structural ana...
Structural temperatures and thermal protection system surface temperatures were measured on the spac...
The aerodynamic heating of a tip-fin controller mounted on a Space Shuttle Orbiter model was studied...
Entry heating flight data and wind tunnel data on the lower wing 50% and 80% Semi-Spans are presente...
The aerothermodynamic performance of the Space Shuttle Orbiter during reentry is assessed from the c...
Entry heating flight data and wind tunnel data on the lower surface centerline are presented in term...
The Space Shuttle orbiter's thermal protection system (TPS), designed mainly on the basis of wind tu...
A structural performance and resizing (SPAR) finite element thermal analysis computer program was us...
A broad base of thermocouple and phase change paint data was assembled and correlated to the nominal...
Heating rate and pressure measurements were obtained on a 25-O space shuttle model in a vacuum chamb...
Aerothermodynamic development flight test data from the first orbital flight test of the Space Trans...
An analytical program is in progress at Rockwell International to revise wing leading edge heating p...
A preliminary analysis of data acquired during the first shuttle orbiter reentry is presented. Heati...
The research for determining the space shuttle aerothermal environment is reported. Brief summaries ...
Conference on aerodynamic heat transfer in space shuttle configurations and procedures and technique...
A structural performance and resizing (SPAR) finite-element computer program and NASA structural ana...
Structural temperatures and thermal protection system surface temperatures were measured on the spac...
The aerodynamic heating of a tip-fin controller mounted on a Space Shuttle Orbiter model was studied...
Entry heating flight data and wind tunnel data on the lower wing 50% and 80% Semi-Spans are presente...
The aerothermodynamic performance of the Space Shuttle Orbiter during reentry is assessed from the c...
Entry heating flight data and wind tunnel data on the lower surface centerline are presented in term...
The Space Shuttle orbiter's thermal protection system (TPS), designed mainly on the basis of wind tu...
A structural performance and resizing (SPAR) finite element thermal analysis computer program was us...
A broad base of thermocouple and phase change paint data was assembled and correlated to the nominal...
Heating rate and pressure measurements were obtained on a 25-O space shuttle model in a vacuum chamb...
Aerothermodynamic development flight test data from the first orbital flight test of the Space Trans...
An analytical program is in progress at Rockwell International to revise wing leading edge heating p...
A preliminary analysis of data acquired during the first shuttle orbiter reentry is presented. Heati...
The research for determining the space shuttle aerothermal environment is reported. Brief summaries ...
Conference on aerodynamic heat transfer in space shuttle configurations and procedures and technique...
A structural performance and resizing (SPAR) finite-element computer program and NASA structural ana...
Structural temperatures and thermal protection system surface temperatures were measured on the spac...
The aerodynamic heating of a tip-fin controller mounted on a Space Shuttle Orbiter model was studied...