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Infrared Spectral Measurement of Space Shuttle GlowThe U.S. Air Force and NASA successfully conducted infrared spectral measurements of the space shuttle glow during STS-39. Preliminary analysis indicates that NO, NO+, OH, and CO produce infrared glow during quiescent orbiter conditions. During orbiter thruster firings the glow intensities in the infrared are enhanced by factors of 10X to 100X with significant changes in spectral distribution. These measurements were obtained with the Spacecraft Kinetic Infrared Test (SKIRT) payload which included a cryogenic infrared circular variable filter infrared spectrometer covering the 0.7 to 5.4 μm wavelength region. Approximately 14,000 spectra of shuttle glow, airglow, aurora, and the orbiter environment were obtained during the eight day mission. The STS-39 Space Shuttle Discovery was launched from the NASA Kennedy Space Center on 28 April 1991 into a 57 deg inclination circular orbit at an altitude of 260 km.
Document ID
19920059059
Acquisition Source
Goddard Space Flight Center
Document Type
Reprint (Version printed in journal)
Authors
M Ahmadjian
(Phillips Laboratory Kirtland AFB, United States)
D E Jennings
(Science Systems and Applications (United States) Lanham, Maryland, United States)
M J Mumma ORCID
(Goddard Space Flight Center Greenbelt, United States)
F Espenak
(Goddard Space Flight Center Greenbelt, United States)
C J Rice
(The Aerospace Corporation El Segundo, California, United States)
R W Russell
(The Aerospace Corporation El Segundo, California, United States)
B D Green
(Physical Sciences (United States) Andover, Massachusetts, United States)
Date Acquired
August 15, 2013
Publication Date
May 22, 1992
Publication Information
Publication: Geophysical Research Letters
Publisher: American Geophysical Union
Volume: 19
Issue: 10
Issue Publication Date: May 22, 1992
ISSN: 0094-8276
e-ISSN: 1944-8007
Subject Category
Spacecraft Design, Testing and Performance
Accession Number
92A41683
Distribution Limits
Public
Copyright
Public Use Permitted.
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