5029 x 3744 px | 42,6 x 31,7 cm | 16,8 x 12,5 inches | 300dpi
Aufnahmedatum:
9. April 2016
Ort:
The Kennedy Space Centre, Merritt Island, Florida, USA.
Weitere Informationen:
The Space Shuttle thermal protection system (TPS) is the barrier that protected the Space Shuttle Orbiter during the searing 1, 650 °C (3, 000 °F) heat of atmospheric re-entry. A secondary goal was to protect from the heat and cold of space while in orbit. The TPS covered essentially the entire orbiter surface, and consisted of seven different materials in varying locations based on amount of required heat protection: Reinforced carbon–carbon (RCC), used in the nose cap, the chin area between the nose cap and nose landing gear doors, the arrowhead aft of the nose landing gear door, and the wing leading edges. Used where reentry temperature exceeded 1, 260 °C (2, 300 °F). High-temperature reusable surface insulation (HRSI) tiles, used on the orbiter underside. Made of coated LI-900 Silica ceramics. Used where reentry temperature was below 1260 °C. Fibrous refractory composite insulation (FRCI) tiles, used to provide improved strength, durability, resistance to coating cracking and weight reduction. Some HRSI tiles were replaced by this type. Flexible Insulation Blankets (FIB), a quilted, flexible blanket-like surface insulation. Used where reentry temperature was below 649 °C (1, 200 °F). Low-temperature Reusable Surface Insulation (LRSI) tiles, formerly used on the u per fuselage, but were mostly replaced by FIB. Used in temperature ranges roughly similar to FIB. Toughened unipiece fibrous insulation (TUFI) tiles, a stronger, tougher tile which came into use in 1996. Used in high and low temperature areas. Felt reusable surface insulation (FRSI). White Nomex felt blankets on the upper payload bay doors, portions of the mid fuselage and aft fuselage sides, portions of the upper wing surface and a portion of the OMS/RCS pods. Used where temperatures stayed below 371 °C (700 °F). Each type of TPS had specific heat protection, impact resistance, and weight characteristics, which determined the locations where it was used and the amount used.
