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Title: Thermal Protection System Sensors
Primary Author: Edward R. Martinez
Secondary Author(s): Robert V. Frampton
Institution: NASA Ames Research Center
Summary: This paper advocates for the development of an aeroshell TPS sensor system to the benefit of all atmospheric reentry missions Agency wide.
Panel Selection: Inner Planets: Mercury, Venus, and the Moon. Mars: Not Phobos and Deimos. Giant Planets: Jupiter, Saturn, Uranus, Neptune, and exoplanets, including rings and magnetic fields, but not their satellites. Satellites: Galilean satellites, Titan, and the other satellites of the giant planets. Primitive Bodies: Asteroids, comets, Phobos, Deimos, Pluto/Charon and other Kuiper belt objects, meteorites, and interplanetary dust.
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These documents have been prepared in coordination with the National Academies of Science in support of the National Academies Planetary Science Decadal Survey. These documents are being made available for information purposes only, and any views and opinions expressed herein do not necessarily state or reflect those of NASA, JPL, or the California Institute of Technology.