Add to ORKGDesign and operation of make wire, light pipe, and spring wire sensors to measure in-flight thermal parameters of ablative reentry vehicle heat shiel
This is a chart for the NASA Ames Instrumentation Workshop scheduled for 16-Sept-2015. The workshop ...
Hemispherical spectral emittance of ablation chars, carbon, and zirconia during atmospheric reentr
Thermal and flow sensor instrumentation was developed for use as an integral part of the space shutt...
Design and development of sensors for measuring ablative changes in space vehicle heat shield during...
Sensors measure surface erosion rate of ablating material in reentry vehicle heat shield. Each senso...
Radioactive isotope technique for heat shield ablation measurement during reentr
Reentry shielding ablation measured by imbedded radioactive isotopes with radiation decto
Design, operation and construction of event recorder for monitoring heat ablation dat
Ablating materials tested at combined radiative and convective heating for manned reentry vehicle he...
Extrait de : 1st European symposium on aerothermodynamics for space vehicles, ESTEC, Noordwijk (The ...
Ablation behavior of heat shield of Apollo command module over wide range of thermal environment
Ability of several ablating materials to reduce surface heat transfer in electric arc heated airstre...
Pyrotechnic-actuated calorimeter for flight research at lunar return velocity /Project Fire
Heat-transfer rates and ablation on blunt flared cylinder in free flight at hypersonic and lower spe...
During all phases of a spacecraft's mission, a Thermal Protection System (TPS) is needed to protect ...
This is a chart for the NASA Ames Instrumentation Workshop scheduled for 16-Sept-2015. The workshop ...
Hemispherical spectral emittance of ablation chars, carbon, and zirconia during atmospheric reentr
Thermal and flow sensor instrumentation was developed for use as an integral part of the space shutt...
Design and development of sensors for measuring ablative changes in space vehicle heat shield during...
Sensors measure surface erosion rate of ablating material in reentry vehicle heat shield. Each senso...
Radioactive isotope technique for heat shield ablation measurement during reentr
Reentry shielding ablation measured by imbedded radioactive isotopes with radiation decto
Design, operation and construction of event recorder for monitoring heat ablation dat
Ablating materials tested at combined radiative and convective heating for manned reentry vehicle he...
Extrait de : 1st European symposium on aerothermodynamics for space vehicles, ESTEC, Noordwijk (The ...
Ablation behavior of heat shield of Apollo command module over wide range of thermal environment
Ability of several ablating materials to reduce surface heat transfer in electric arc heated airstre...
Pyrotechnic-actuated calorimeter for flight research at lunar return velocity /Project Fire
Heat-transfer rates and ablation on blunt flared cylinder in free flight at hypersonic and lower spe...
During all phases of a spacecraft's mission, a Thermal Protection System (TPS) is needed to protect ...
This is a chart for the NASA Ames Instrumentation Workshop scheduled for 16-Sept-2015. The workshop ...
Hemispherical spectral emittance of ablation chars, carbon, and zirconia during atmospheric reentr
Thermal and flow sensor instrumentation was developed for use as an integral part of the space shutt...