| タイトル | External Tank (ET) Bipod Fitting Bolted Attachment Locking Insert Performance |
| 本文（外部サイト） | http://hdl.handle.net/2060/20080007518 |
| 著者（英） | Larsen, Curtis E.; Raju, Ivatury S.; Elliott, Kenny B.; Wilson, Tim R.; McManamen, John |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 2008-01-01 |
| 言語 | eng |
| 内容記述 | Following STS-107, the External Tank (ET) Project implemented corrective actions and configuration changes at the ET bipod fitting. Among the corrective actions, the existing bolt lock wire which provided resistance to potential bolt rotation was removed. The lock wire removal was because of concerns with creating voids during foam application and potential for lock wire to become debris. The bolts had been previously lubricated to facilitate assembly but, because of elimination of the lock wire, the ET Project wanted to enable the locking feature of the insert. Thus, the lubrication was removed from bolt threads and instead applied to the washer under the bolt head. Lubrication is necessary to maximize joint pre-load while remaining within the bolt torque specification. The locking feature is implemented by thread crimping in at four places in the insert. As the bolt is torqued into the insert the bolt threads its way past the crimped parts of the insert. This provides the locking of the bolt, as torque is required to loosen the joint after clamping. |
| NASA分類 | Spacecraft Design, Testing and Performance |
| レポートNO | L-19439
NASA/TM-2008-215099
NESC-RP-06-53/06-032-E |
| 権利 | No Copyright |
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