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A millimeter wave technique for measuring ice thickness on the Space Shuttle's external tankA solution is presented for detecting and measuring ice that can form on the spray-on foam insulation protecting Space Shuttle fueltanks. The method involves the measurement of the emission properties of the fueltank with a mm-wave radiometer. Emission from the insulated panel is measured for the case of insulation with the original rough surface and the case of insulation sanded down to have a smooth surface. The radiative transfer calculations are facilitated by using a smooth surface, and experimental evidence demonstrates the effective and accurate prediction of ice thickness on the smooth surface. The panel with a rough surface is measured, and the emmision levels are higher than those predicted by model calculations. Sensitivity to ice thickness is similar in both situations in spite of the bias introduced by the rough surface.
Document ID
19920034585
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
External Source(s)
Authors
Kendra, John E.
(Michigan Univ. Ann Arbor, MI, United States)
Ulaby, Fawwaz T.
(Michigan, University Ann Arbor, United States)
Wu, Steve
(NASA Stennis Space Center Bay Saint Louis, MS, United States)
Date Acquired
August 15, 2013
Publication Date
December 1, 1991
Publication Information
Publication: International Journal of Infrared and Millimeter Waves
Volume: 12
ISSN: 0195-9271
Subject Category
Ground Support Systems And Facilities (Space)
Report/Patent Number
ISSN: 0195-9271
Accession Number
92A17209
Distribution Limits
Public
Copyright
Other

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