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Extreme Ultraviolet Variability Experiment (EVE) on the Solar Dynamics Observatory (SDO): Overview of Science Objectives, Instrument Design, Data Products, and Model DevelopmentsThe highly variable solar extreme ultraviolet (EUV) radiation is the major energy input to the Earth's upper atmosphere, strongly impacting the geospace environment, affecting satellite operations, communications, and navigation. The Extreme ultraviolet Variability Experiment (EVE) onboard the NASA Solar Dynamics Observatory (SDO) will measure the solar EUV irradiance from 0.1 to 105 nm with unprecedented spectral resolution (0.1 nm), temporal cadence (ten seconds), and accuracy (20%). EVE includes several irradiance instruments: The Multiple EUV Grating Spectrographs (MEGS)-A is a grazingincidence spectrograph that measures the solar EUV irradiance in the 5 to 37 nm range with 0.1-nm resolution, and the MEGS-B is a normal-incidence, dual-pass spectrograph that measures the solar EUV irradiance in the 35 to 105 nm range with 0.1-nm resolution. To provide MEGS in-flight calibration, the EUV SpectroPhotometer (ESP) measures the solar EUV irradiance in broadbands between 0.1 and 39 nm, and a MEGS-Photometer measures the Sun s bright hydrogen emission at 121.6 nm. The EVE data products include a near real-time space-weather product (Level 0C), which provides the solar EUV irradiance in specific bands and also spectra in 0.1-nm intervals with a cadence of one minute and with a time delay of less than 15 minutes. The EVE higher-level products are Level 2 with the solar EUV irradiance at higher time cadence (0.25 seconds for photometers and ten seconds for spectrographs) and Level 3 with averages of the solar irradiance over a day and over each one-hour period. The EVE team also plans to advance existing models of solar EUV irradiance and to operationally use the EVE measurements in models of Earth s ionosphere and thermosphere. Improved understanding of the evolution of solar flares and extending the various models to incorporate solar flare events are high priorities for the EVE team.
Document ID
20120012554
Acquisition Source
Goddard Space Flight Center
Document Type
Reprint (Version printed in journal)
Authors
Woods, T. N.
(Colorado Univ. Boulder, CO, United States)
Eparvier, F. G.
(Colorado Univ. Boulder, CO, United States)
Hock, R.
(Colorado Univ. Boulder, CO, United States)
Jones, A. R.
(Colorado Univ. Boulder, CO, United States)
Woodraska, D.
(Colorado Univ. Boulder, CO, United States)
Judge, D.
(University of Southern California Los Angeles, CA, United States)
Didkovsky, L.
(University of Southern California Los Angeles, CA, United States)
Lean, J.
(Naval Research Lab. Washington, DC, United States)
Mariska, J.
(Naval Research Lab. Washington, DC, United States)
Warren, H.
(Naval Research Lab. Washington, DC, United States)
McMullin, D.
(Space Systems Research Corp. Alexandria, VA, United States)
Chamberlin, P.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Berthiaume, G.
(Massachusetts Inst. of Tech. Lexington, MA, United States)
Bailey, S.
(Virginia Tech Blacksburg, VA, United States)
Fuller-Rowell, T.
(Colorado Univ. Boulder, CO, United States)
Sojka, J.
(Utah State Univ. Logan, UT, United States)
Tobiska, W. K.
(Space Environment Technologies Pacific Palisades, CA, United States)
Viereck, R.
(National Oceanic and Atmospheric Administration Boulder, CO, United States)
Date Acquired
August 26, 2013
Publication Date
January 12, 2010
Publication Information
Publication: Solar Physics
Publisher: Springer-Verlag G.m.b.H. and Co. K.G.
Volume: 275
Issue: 2-Jan
Subject Category
Spacecraft Instrumentation And Astrionics
Report/Patent Number
GSFC.JA.01212.2012
Funding Number(s)
CONTRACT_GRANT: NAS5-02140
Distribution Limits
Public
Copyright
Public Use Permitted.
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