TY - GEN
T1 - Real-time space materials degradation monitor using ellipsometer
AU - Machlab, Hassanayn
AU - Synowicki, R. A.
AU - Ducharme, Steven P.
AU - Snyder, Paul G.
AU - Woollam, John A.
N1 - Publisher Copyright:
© 1995 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.
PY - 1995
Y1 - 1995
N2 - NASA has a need for a simple, low-cost, compact, lightweight and rugged instrument to monitor materials degradation in the atomic oxygen (AO) environment of low Earth orbit (LEO). The purpose of the reported SBIR contract work was to build a space-fly able ellipsometer to meet these needs. The small modulation ellipsometer (SME) built uses polarization modulation and an arrangement of optical elements permitting simultaneous and continuous measurement of the ellipsometric parameters without reference to external calibration or to elaborate alignment procedures. This ellipsometer directly measures the most significant errors in system alignment that perhaps might occur at initial construction or during space launch. This ellipsometer contains no moving parts, requires only low electrical power, can work in vacuum conditions, and could be flight-qualified to be operable in space.
AB - NASA has a need for a simple, low-cost, compact, lightweight and rugged instrument to monitor materials degradation in the atomic oxygen (AO) environment of low Earth orbit (LEO). The purpose of the reported SBIR contract work was to build a space-fly able ellipsometer to meet these needs. The small modulation ellipsometer (SME) built uses polarization modulation and an arrangement of optical elements permitting simultaneous and continuous measurement of the ellipsometric parameters without reference to external calibration or to elaborate alignment procedures. This ellipsometer directly measures the most significant errors in system alignment that perhaps might occur at initial construction or during space launch. This ellipsometer contains no moving parts, requires only low electrical power, can work in vacuum conditions, and could be flight-qualified to be operable in space.
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M3 - Conference contribution
AN - SCOPUS:84959255566
SN - 9781623565244
T3 - 1995 Space Programs and Technologies Conference
SP - 1
EP - 5
BT - Space Programs and Technologies Conference
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - Space Programs and Technologies Conference, 1995
Y2 - 26 September 1995 through 28 September 1995
ER -