Space Shuttle Thermal Protection System
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High Quality Content by WIKIPEDIA articles! The Space Shuttle thermal protection system (TPS) is the barrier that protects the Space Shuttle Orbiter during the searing 1650 °C (3000 °F) heat of atmospheric reentry. A secondary goal is to protect from the heat and cold of space while on orbit.[1] The TPS covers essentially the entire orbiter surface, and consists of seven different materials in varying locations based on amount of required heat protection: Reinforced carbon-carbon (RCC), used in the nose cap and wing leading edges. Used where reentry temperature exceeds 1260 °C (2300 °F).

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High Quality Content by WIKIPEDIA articles! The Space Shuttle thermal protection system (TPS) is the barrier that protects the Space Shuttle Orbiter during the searing 1650 °C (3000 °F) heat of atmospheric reentry. A secondary goal is to protect from the heat and cold of space while on orbit.[1] The TPS covers essentially the entire orbiter surface, and consists of seven different materials in varying locations based on amount of required heat protection: Reinforced carbon-carbon (RCC), used in the nose cap and wing leading edges. Used where reentry temperature exceeds 1260 °C (2300 °F).