LDEF (Postflight), NASA history collection

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LDEF (Postflight), NASA history collection

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Summary

LDEF (Postflight) The LDEF structure is shown, from a rear oblique angle, mounted on the LDEF Assembly and Transport System (LATS)in the SAEF II at the KSC after deintegration of experiments from the LDEF. The LDEF structure is a welded / bolted assembly fabricated from aluminum alloy 6061-T6 extrusions, forgings, tubing and plate materials and assembled with stainless steel fasteners. The eight (8) internal tubular diagonals between the center ring structure and the two end frames provides torsional stiffness to the structure. The passive grapple tray remains mounted in the LDEF C01 location. A thermal control panel, adjacent to the LDEF experiment F06 location, was removed prior to experiment deintegration in preparation for configuring the LDEF for rotation. A light brown discoloration can be seen on the anodized aluminum thermal control panels on the LDEF Space end. Discolorations are also visible on surfaces of the LDEF longeron and intercostal structures that were exposed during the mission.
NASA Identifier: L92-17921 KSC-390C-2366.06

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Date

1990
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Source

Defense Visual Information Distribution Service
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