| タイトル | Life considerations of the shuttle orbiter densified-tile thermal protection system |
| 本文（外部サイト） | http://hdl.handle.net/2060/19840002092 |
| 著者（英） | Sawyer, J. W.; Cooper, P. A. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1983-10-01 |
| 言語 | eng |
| 内容記述 | The Shuttle orbiter themal protection system (TPS) incorporates ceramic reusable surface insulation tiles bonded to the orbiter substructure through a strain isolation pad. Densification of the bonding surface of the tiles increases the static strength of the tiles. The densification proces does not, however, necessarily lead to an equivalent increase in fatigue strength. Investigation of the expected lifetime of densified tile TPS under both sinusoidal loading and random loading simulating flight conditions indicates that the strain isolation pads are the weakest components of the TPS under fatigue loading. The felt pads loosen under repetitive loading and, in highly loaded regions, could possibly cause excessive step heights between tiles causing burning of the protective insulation between tiles. A method of improving the operational lifetime of the TPS by using a strain isolation pad with increased stiffness is presented as is the consequence of the effect of increased stiffness on the tile inplane strains and transverse stresses. |
| NASA分類 | SPACE TRANSPORTATION |
| レポートNO | 84N10159 |
| 権利 | No Copyright |
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