Add to ORKGAblation behavior of heat shield of Apollo command module over wide range of thermal environment
Tests were performed to demonstrate the feasibility of a new method of measuring surface recession o...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/90680/1/AIAA-2011-3125-594.pd
I The Initial results of the application of special optical techniques to high-temperature emittance...
Hypersonic spacecraft reentering the earth's atmosphere encounter extreme heat due to atmospheric fr...
Emittance as function of temperature for five ablative materials used as rocket engine liner
Results which were achieved by a seven-wavelength pyrometer last year are reported in this paper. Th...
Bibliography on emittance of high temperature materials including refractory materials, ceramics, ca...
Thermophysical property data for ablation materials - aerodynamic heating of low density phenolic ny...
Design and operation of make wire, light pipe, and spring wire sensors to measure in-flight thermal ...
Emission spectroscopy measurements in the post-shock layer in front of low density ablative material...
Design and development of sensors for measuring ablative changes in space vehicle heat shield during...
Hemispherical total emittance and normal solar absorptance of selected materials at temperature rang...
Energy transfer in pyrolysis product flow through char layer of nylon phenolic resin ablato
Vehicles entering planetary atmospheres at high speed require an ablative heat shield in order to wi...
Ablation behavior of heat shield of Apollo command module over wide range of thermal environment
Tests were performed to demonstrate the feasibility of a new method of measuring surface recession o...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/90680/1/AIAA-2011-3125-594.pd
I The Initial results of the application of special optical techniques to high-temperature emittance...
Hypersonic spacecraft reentering the earth's atmosphere encounter extreme heat due to atmospheric fr...
Emittance as function of temperature for five ablative materials used as rocket engine liner
Results which were achieved by a seven-wavelength pyrometer last year are reported in this paper. Th...
Bibliography on emittance of high temperature materials including refractory materials, ceramics, ca...
Thermophysical property data for ablation materials - aerodynamic heating of low density phenolic ny...
Design and operation of make wire, light pipe, and spring wire sensors to measure in-flight thermal ...
Emission spectroscopy measurements in the post-shock layer in front of low density ablative material...
Design and development of sensors for measuring ablative changes in space vehicle heat shield during...
Hemispherical total emittance and normal solar absorptance of selected materials at temperature rang...
Energy transfer in pyrolysis product flow through char layer of nylon phenolic resin ablato
Vehicles entering planetary atmospheres at high speed require an ablative heat shield in order to wi...
Ablation behavior of heat shield of Apollo command module over wide range of thermal environment
Tests were performed to demonstrate the feasibility of a new method of measuring surface recession o...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/90680/1/AIAA-2011-3125-594.pd