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Lunar Glovebox Balance with Wireless TechnologyThe most important equipment required for processing lunar samples is a high-quality mass balance for maintaining accurate weight inventory, security, and scientific study. After careful review, a Curation Office memo by Michael Duke in 1978 chose the Mettler PL200 to be used for sample weight measurements inside the gloveboxes (Fig. 3). These commercial off-the-shelf (COTS) balances did not meet the strict accepted material requirements in the Lunar lab. As a result, each balance housing, weighing pan, and wiring was custom retrofitted to meet Lunar Operating Procedure (LOP) 54 requirements [for material construction restrictions]. The original design drawings for the custom housings, readout support stands, and wiring were done by the JSC engineering directorate. The 1977- 1978 schematics, drawings, and files are now housed in the curation Data Center. Per the design specifications, the housing was fabricated from aluminum grade 6061 T6, seamless welds, and anodized per MIL-A-8625 type I, class I. The balance feet were TFE Teflon and any required joints were sealed with Viton A gaskets. The readout display and support stands outside the glovebox were fabricated from 300 series stainless steel with #4 finish and mounted to the glovebox with welded bolts. Wire harnesses that linked the balance with the outside display and power were encapsulated with TFE Teflon and transported through custom Deutsch wire bulk head pass-through systems from inside to outside the glovebox. These Deutsch connectors were custom fabricated with 316L stainless steel bodies, Viton A O-rings, aluminum 6061 with electroless nickel plating, Teflon (replacing the silicone), and gold crimp connectors (no soldering). Many of the Deutsch connectors may have been used in the Apollo program high vacuum complex in building 37 and date to about 1968 to 1970.
Document ID
20200001581
Acquisition Source
Johnson Space Center
Document Type
Technical Memorandum (TM)
Authors
Zeigler, Ryan A.
(NASA Johnson Space Center Houston, TX, United States)
McCubbin, Francis M.
(NASA Johnson Space Center Houston, TX, United States)
Calaway, Michael J.
(Jacobs Engineering Group Houston, TX, United States)
Date Acquired
March 13, 2020
Publication Date
June 12, 2019
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA/TM-2019-220206
JSC-E-DAA-TN68094
Report Number: NASA/TM-2019-220206
Report Number: JSC-E-DAA-TN68094
Funding Number(s)
CONTRACT_GRANT: NNJ13HA01C
Distribution Limits
Public
Copyright
Public Use Permitted.
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