REG NASA-LLIS-3759-2011 Lessons Learned - Space Shuttle High-Density Electrical Connector Retest.pdf
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1、Public Lessons Learned Entry: 3759 Lesson Info: Lesson Number: 3759 Lesson Date: 2010-08-25 Submitting Organization: KSC Submitted by: Annette Pitt Subject: Space Shuttle High-Density Electrical Connector Retest Abstract: Thousands of electrical connectors are used on the Space Shuttle Orbiter to al
2、low quick connection and disconnection of electrical circuits for maintenance, modification, inspection, or troubleshooting. NLS connectors (NLS is the prefix to the connector part number) are a frequently used type, are procured according to 40M38277 Marshall Space Flight Center (MSFC) specificatio
3、n, and are similar in construction to MIL-C-38999, Series II, connectors. NLS connectors are commonly referred to as high-density connectors because of their generally high number of small contacts per connector (up to 128 size 22D contacts in a single connector). From a design perspective, 128-pin
4、NLS connectors offer space and weight advantages but are challenging from a vehicle-processing perspective. Pictures of the front and back of an NLS connector are attached. The front view shows a bent pin. The back view shows the density of the wiring attached to the connector. Description of Drivin
5、g Event: Thousands of electrical connectors are used on the Space Shuttle Orbiter to allow quick connection and disconnection of electrical circuits for maintenance, modification, inspection, or troubleshooting. NLS connectors are procured according to MSFC specification 40M38277 and are similar in
6、construction to MIL-C-38999, Series II, connectors. NLS connectors are commonly referred to high-density connectors because of their generally high number of small contacts per connector (up to 128 size 22D contacts in a single connector). From a design perspective, 128-pin NLS connectors offer spac
7、e and weight advantages but are challenging from a vehicle processing perspective. First, the contacts of high-density connectors are more susceptible to bending during mating and demating than those of lower-density connectors. If the connector is damaged beyond repair, each connector contact must
8、be depinned and repinned a labor-intensive operation. Second, demating and reworking connectors have a significant effect on system-level retesting. According to the Orbiter Maintenance Requirements and Specifications Document (OMRSD), when a connector is demated, each pin must be functionally rever
9、ified after the connector is remated before the next mission. This requirement was imposed to detect bent or recessed contacts or other anomalies that could otherwise go undetected until the function was used during flight. In addition, the OMRSD requires that all replaced connectors be continuity-t
10、ested prior to power-up to verify that they were pinned appropriately. This requirement was imposed to ensure that flight hardware was not inadvertently electrically damaged because of a missed pin. Meeting these requirements for high-density connectors can be challenging, and the retesting alone ca
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