You have requested a machine translation of selected content from our databases. This functionality is provided solely for your convenience and is in no way intended to replace human translation. Neither SPIE nor the owners and publishers of the content make, and they explicitly disclaim, any express or implied representations or warranties of any kind, including, without limitation, representations and warranties as to the functionality of the translation feature or the accuracy or completeness of the translations.
Translations are not retained in our system. Your use of this feature and the translations is subject to all use restrictions contained in the Terms and Conditions of Use of the SPIE website.
26 September 2013Performance results from in-flight commissioning of the Juno Ultraviolet Spectrograph (Juno-UVS)
T. K. Greathouse,1 G. R. Gladstone,1 M. W. Davis,1 D. C. Slater,1 M. H. Versteeg,1 K. B. Persson,1 B. C. Walther,1 G. S. Winters,1 S. C. Persyn,1 J. S. Eterno1
We present a description of the Juno ultraviolet spectrograph (Juno-UVS) and results from its in-flight commissioning
performed between December 5th and 13th 2011 and its first periodic maintenance between October 10th and 12th 2012.
Juno-UVS is a modest power (9.0 W) ultraviolet spectrograph based on the Alice instruments now in flight aboard the
European Space Agency’s Rosetta spacecraft, NASA’s New Horizons spacecraft, and the LAMP instrument aboard
NASA’s Lunar Reconnaissance Orbiter. However, unlike the other Alice spectrographs, Juno-UVS sits aboard a spin
stabilized spacecraft. The Juno-UVS scan mirror allows for pointing of the slit approximately ±30° from the spacecraft
spin plane. This ability gives Juno-UVS access to half the sky at any given spacecraft orientation. The planned 2 rpm
spin rate for the primary mission results in integration times per 0.2° spatial resolution element per spin of only ~17 ms.
Thus, for calibration purposes, data were retrieved from many spins and then remapped and co-added to build up
exposure times on bright stars to measure the effective area, spatial resolution, scan mirror pointing positions, etc. The
primary job of Juno-UVS will be to characterize Jupiter’s UV auroral emissions and relate them to in-situ particle
measurements. The ability to point the slit will make operations more flexible, allowing Juno-UVS to observe the
atmospheric footprints of magnetic field lines through which Juno flies, giving a direct connection between energetic
particle measurements on the spacecraft and the far-ultraviolet emissions produced by Jupiter’s atmosphere in response
to those particles.
The alert did not successfully save. Please try again later.
T. K. Greathouse, G. R. Gladstone, M. W. Davis, D. C. Slater, M. H. Versteeg, K. B. Persson, B. C. Walther, G. S. Winters, S. C. Persyn, J. S. Eterno, "Performance results from in-flight commissioning of the Juno Ultraviolet Spectrograph (Juno-UVS)," Proc. SPIE 8859, UV, X-Ray, and Gamma-Ray Space Instrumentation for Astronomy XVIII, 88590T (26 September 2013); https://doi.org/10.1117/12.2024537