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- W22460893 abstract "A mission close to the sun is only possible if new spacecraft technologies can be developed and incorporated into a state‐of‐the‐art spacecraft concept. The perihelion goal of 4 solar radii requires a shielded spacecraft that can tolerate the almost 3000 suns solar flux while maintaining the electronics components at room temperature. In addition, the shield surface should sublimate at a rate of less than 3mg/s at perihelion. Many shield configuration designs have been studied and the most promising is a parabolic shape that functions as both a shield and a large high gain antenna. The shield material chosen for this design is a carbon‐carbon material with highly emissive surface properties. A mission requirement for a high telecommunications power stems from the expected interference when attempting to transmit data through the solar corona. It is expected that the large carbon‐carbon shield/antenna will have a high power gain even at high temperatures and will return adequate telemetry at the X‐band rad..." @default.
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- W22460893 date "1996-01-01" @default.
- W22460893 modified "2023-09-26" @default.
- W22460893 title "Solar probe technology challenges" @default.
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- W22460893 doi "https://doi.org/10.1063/1.50003" @default.
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