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A Study to Analyze the Permeation of High Density Gases and Propellant Vapors Through Single Layer Teflon or Teflon Structure Materials and LaminationsThis report contains the results of a fifteen month analytical and experimental study of the leakage rate of the pressurant gases (N2, He) and the propellant vapors (N2O4,N2H4) through bladder structures consisting of two layers of Teflon separated by a metallic foil diffusion barrier containing microscopic or larger holes. Results were obtained for the steady state leakage rate through circular holes and long rectangular openings in the barrier for arbitrary thicknesses of the two Teflon layers. The effect of hole shape and relative hole position on the leakage rate were studied. The transient problem was analyzed and it was shown that steady state calculations are adequate for estimating the leakage rate. A computer program entitled "Diffusion Analyzer Program" was developed to calculate the leakage rate, both transient and steady state. Finally, the analytical results were compared to experimentally determined values of the leakage rate through a model laminated bladder structure. The results of the analysis are in good agreement with experiment. The experimental effort (Part II of the Bladder Permeation Program) measured the solubility, diffusion coefficient and permeability of helium, nitrogen and nitrogen tetroxide vapor through Teflon TFE and FEP membranes. Data were obtained in the temperature range of 25 to 100 C at pressures ranging from near vacuum to about 20 atmospheres. Results of the experimental effort were compared with the limited data previously reported. As a verification to the applicability of results to actual bladder systems, counter diffusion tests were performed with a laminated sample containing aluminum foil with a selected group of holes.
Document ID
20010082538
Acquisition Source
Jet Propulsion Laboratory
Document Type
Contractor or Grantee Report
Authors
Johnson, R. L.
(TRW Systems Group Redondo Beach, CA United States)
Young, Donald L.
Date Acquired
September 7, 2013
Publication Date
October 25, 1967
Subject Category
Propellants And Fuels
Report/Patent Number
TRW-07282-6016-R000-Vol-1
Report Number: TRW-07282-6016-R000-Vol-1
Funding Number(s)
CONTRACT_GRANT: NAS7-505
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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