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Visible light emission excited by interaction of Space Shuttle exhaust with the atmosphereGround-based video photography of firings of Space Shuttle Primary Reaction Control System (PRCS) engines show optical emissions extending nearly 4 km form the vehicle after steady state is reached. The total intensity and spatial distribution of these emissions depend on the angle between the spacecraft velocity vector and the engine exhaust axis. Candidate sources for this radiation are reviewed and the conclusion is reached that it is most likely due to vibrationally excited OH, formed by the reaction of fast ambient O atoms and H2O molecules in the exhaust.
Document ID
19910031770
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Murad, E.
(Air Force Geophysics Lab. Hanscom AFB, MA, United States)
Knecht, D. J.
(Air Force Geophysics Lab. Hanscom AFB, MA, United States)
Viereck, R. A.
(Air Force Geophysics Lab. Hanscom AFB, MA, United States)
Pike, C. P.
(USAF, Geophysics Laboratory, Hanscom AFB MA, United States)
Kofsky, I. L.
(Air Force Geophysics Lab. Hanscom AFB, MA, United States)
Trowbridge, C. A.
(Air Force Geophysics Lab. Hanscom AFB, MA, United States)
Rall, D. L. A.
(PhotoMetrics, Inc. Woburn, MA, United States)
Ashley, G.
(Air Force Geophysics Lab. Hanscom AFB, MA, United States)
Twist, L.
(Avco Research Laboratory Puunene, HI, United States)
Blaha, J. E.
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
August 15, 2013
Publication Date
November 1, 1990
Publication Information
Publication: Geophysical Research Letters
Volume: 17
ISSN: 0094-8276
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
91A16393
Distribution Limits
Public
Copyright
Other

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