Add to ORKGResults are presented from an investigation to determine the effects of fabrication-induced defects ...
Radio frequency transmission characteristics of ablation materials for planetary entry vehicle heat ...
Entering a planetary atmosphere is one of the most claim missions as the space probe faces a loss of...
Reentry shielding ablation measured by imbedded radioactive isotopes with radiation decto
Sensors measure surface erosion rate of ablating material in reentry vehicle heat shield. Each senso...
Design and development of sensors for measuring ablative changes in space vehicle heat shield during...
Prepared at the Manned Spacecraft Center, Houston, Tex."March 1966"--Cover.Includes bibliographical ...
Design, operation and construction of event recorder for monitoring heat ablation dat
Design and operation of make wire, light pipe, and spring wire sensors to measure in-flight thermal ...
Quantifying the thermal response of a heat shield is a key step in the design of a spacecraft to ens...
Reentry radiation is one of the key phenomena to take into account while designing an Entry Descent ...
Effect of chemical properties of pyrolysis gases on heat shield mass required for lifting reentry ve...
During all phases of a spacecraft's mission, a Thermal Protection System (TPS) is needed to protect ...
International audienceReentry radiation is one of the key phenomena to take into account while desig...
Methods and techniques for monitoring critical heat shield parameters during spacecraft reentr
Results are presented from an investigation to determine the effects of fabrication-induced defects ...
Radio frequency transmission characteristics of ablation materials for planetary entry vehicle heat ...
Entering a planetary atmosphere is one of the most claim missions as the space probe faces a loss of...
Reentry shielding ablation measured by imbedded radioactive isotopes with radiation decto
Sensors measure surface erosion rate of ablating material in reentry vehicle heat shield. Each senso...
Design and development of sensors for measuring ablative changes in space vehicle heat shield during...
Prepared at the Manned Spacecraft Center, Houston, Tex."March 1966"--Cover.Includes bibliographical ...
Design, operation and construction of event recorder for monitoring heat ablation dat
Design and operation of make wire, light pipe, and spring wire sensors to measure in-flight thermal ...
Quantifying the thermal response of a heat shield is a key step in the design of a spacecraft to ens...
Reentry radiation is one of the key phenomena to take into account while designing an Entry Descent ...
Effect of chemical properties of pyrolysis gases on heat shield mass required for lifting reentry ve...
During all phases of a spacecraft's mission, a Thermal Protection System (TPS) is needed to protect ...
International audienceReentry radiation is one of the key phenomena to take into account while desig...
Methods and techniques for monitoring critical heat shield parameters during spacecraft reentr
Results are presented from an investigation to determine the effects of fabrication-induced defects ...
Radio frequency transmission characteristics of ablation materials for planetary entry vehicle heat ...
Entering a planetary atmosphere is one of the most claim missions as the space probe faces a loss of...