The Low-Earth Orbit Flight Test of an Inflatable Decelerator (LOFTID) will test Hyper-sonic Inflatable Aerodynamic Decelerator (HIAD) technology. Temperature measurements are taken across the vehicle to address a Level 1 mission requirement regarding performance of the Flexible Thermal Protection System (F-TPS). Temperature measurements are made using dozens of thermocouples (TCs) embedded within the F-TPS at different depths and various locations shown in Figure 1.
Electrical Shorting of Thermocouples in Atmospheric Entry Applications
17th International Planetary Probe Workshop (IPPW 2020) ; 2020 ; Monterey, CA, US
Aufsatz (Konferenz)
Keine Angabe
Englisch
4300° F thermocouples for re-entry vehicle applications -- 1
Engineering Index Backfile | 1963
|4300 F Thermocouples for Re-Entry Vehicle Applications Part II
SAE Technical Papers | 1963
|4300°F Thermocouples for Re-entry Vehicle Applications – Part I
SAE Technical Papers | 1963
|NTIS | 1981
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