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Demonstration of rapid and sensitive module leak certification for Space Station FreedomA leak detection and quantification demonstration using perflurocarbon tracer (PFT) technology was successfully performed at the NASA Marshall Space Flight Center on January 25, 1991. The real-time Dual Trap Analyzer (DTA) at one-half hour after the start of the first run gave an estimated leak rate of 0.7 mL/min. This has since been refined to be 1.15 (+ or -) 0.09 mL/min. The leak rates in the next three runs were determined to be 9.8 (+ or -) 0.7, -0.4 (+ or -) 0.3, and 76 (+ or -) 6 mL/min, respectively. The theory on leak quantification in the steady-state and time-dependent modes for a single zone test facility was developed and applied to the above determinations. The laboratory PFT analysis system gave a limit-of-detection (LOD) of 0.05 fL for ocPDCH. This is the tracer of choice and is about 100-fold better than that for the DTA. Applied to leak certification, the LOD is about 0.00002 mL/s (0.000075 L/h), a 5 order-of-magnitude improvement over the original leak certification specification. Furthermore, this limit can be attained in a measurement period of 3 to 4 hours instead of days, weeks, or months. A new Leak Certification Facility is also proposed to provide for zonal (three zones) determination of leak rates. The appropriate multizone equations, their solutions, and error analysis have already been derived. A new concept of seal-integrity certification has been demonstrated for a variety of controlled leaks in the range of module leak testing. High structural integrity leaks were shown to have a linear dependence of flow on (Delta)p. The rapid determination of leak rates at different pressures is proposed and is to be determined while subjecting the module to other external force-generating parameters such as vibration, torque, solar intensity, etc.
Document ID
19920075885
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Dietz, R. N.
(Brookhaven National Lab. Upton, NY, United States)
Goodrich, R. W.
(Brookhaven National Lab. Upton, NY, United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1991
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
BNL-47242
DE92-014168
NAS 1.26:186401
NASA-CR-186401
Report Number: BNL-47242
Report Number: DE92-014168
Report Number: NAS 1.26:186401
Report Number: NASA-CR-186401
Accession Number
92N71009
Funding Number(s)
CONTRACT_GRANT: DE-AC02-76CH-00016
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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