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    High-temperature Reusable Surface Insulation (HRSI) is refractory ceramic material used as the basis of the heat shielding of the Space Shuttle. HRSI is refined from sand to form 99.8% (high purity) silica amorphous fibre. Raw HRSI must be combined with a silica-based binding agent & water before sintering.


        HRSI
            Properties of HRSI

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    Properties of HRSI

      Resilient to thermal shock - HRSI tiles can withstand a transition from an environment (1200 degrees Celsius) to full immersion in cold water without sustaining any structural damage.
      Rapid Heat Dissipation - Hot test samples may be handled with an ungloved hand seconds after water quenching, even while the core of the tile still glows red hot.
      Acoustic stress resilience - HRSI tiles can withstand acoustic levels of >165 dB without experiencing structural failure.
      Lack of strength/Porous - HRSI tiling is only 10% material, with the remaining 90% representing void (pores in the material). This form is the cause of the material's excellent refractory behaviour but leads to a lack of tensile strength. The material is also porous as a result.


    HRSI is used in conjunction with stronger, waterproof materials in the Space Shuttle heatshielding to give a balance of strength & resistance to the high re-entry temperatures experienced in Earth's upper atmosphere.

    HRSI is primarily designed to withstand transition from areas of extremely low temperature (the void of space, about -270 degrees Celsius) to the high temperatures of re-entry (caused by friction between the gases of the upper atmosphere & the hull of the Space Shuttle, typically around 1600 degrees Celsius).


     
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    This article is licensed under the GNU Free Documentation License [copyleft]. It uses material from the Wikipedia article "HRSI". link