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Error in Dasibi flight measurements of atmospheric ozone due to instrument wall-lossTheory suggests that in laminar flow the percent loss of a trace constituent to the walls of a measuring instrument varies as P to the -2/3, where P is the total gas pressure. Preliminary laboratory ozone wall-loss measurements confirm this P to the -2/3 dependence. Accurate assessment of wall-loss is thus of particular importance for those balloon-borne instruments utilizing laminar flow at ambient pressure, since the ambient pressure decreases by a factor of 350 during ascent to 40 km. Measurements and extrapolations made for a Dasibi ozone monitor modified for balloon flight indicate that the wall-loss error at 40 km was between 6 and 30 percent and that the wall-loss error in the derived total ozone column-content for the region from the surface to 40 km altitude was between 2 and 10 percent. At 1000 mb, turbulence caused an order of magnitude increase in the Dasibi wall-loss.
Document ID
19820028330
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Ainsworth, J. E.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Hagemeyer, J. R.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Reed, E. I.
(NASA Goddard Space Flight Center Laboratory for Planetary Atmospheres, Greenbelt, MD, United States)
Date Acquired
August 10, 2013
Publication Date
October 1, 1981
Publication Information
Publication: Geophysical Research Letters
Volume: 8
Subject Category
Geophysics
Accession Number
82A11865
Distribution Limits
Public
Copyright
Other

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