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RPW_In_situ_normal_Radio_burstThe RPWI In-situ_normal + Radio_burst mode: - Makes continuous In-situ_normal mode measurement. In addtion to in-situ modes, In-situ_normal mode adds short durations snapshots if electric and magnetic fields at higher frequencies (LF – 763 smpl/s, MF - 50 ksmpl/s and HF - 312 ksmpl/s - Makes full plasma wave measurements and high-time resolution monitoring up to 1.6MHz as well as cover the low frequency and DC electric field and density measurements.RPWI
RPW_IN_SITU_NORMAL_RADIO_FULLThe RPWI In-situ_normal + Radio_Full mode: - Makes continuous In-situ_normal mode measurement. In addtion to in-situ modes, In-situ_normal mode adds short durations snapshots if electric and magnetic fields at higher frequencies (LF – 763 smpl/s, MF - 50 ksmpl/s and HF - 312 ksmpl/s - Makes detailed radio emissions from Jupiter as well as moons (Ganymede, Callisto, Europa). Will also support RIME measurements, giving the background natural radio emissions. Monitor the radio emission spectrum as well as polarization.RPWI
RPW_In_situ_normal_Radar_mode_3The RPWI In-situ_normal + Radio_mode_3 mode: - Makes continuous In-situ_normal mode measurement. In addtion to in-situ_slows modes, In-situ_normal mode adds short durations snapshots if electric and magnetic fields at higher frequencies (LF – 763 smpl/s, MF - 50 ksmpl/s and HF - 312 ksmpl/s - Radio mode TBDRPWI
RPW_In_situ_slow_Radio_burstThe RPWI In-situ_slow + Radio_burst mode: - Makes continuous In-situ_slow mode measurement, the basic in-situ modes; - Makes full plasma wave measurements and high-time resolution monitoring up to 1.6MHz as well as cover the low frequency and DC electric field and density measurements.RPWI
RPW_IN_SITU_SLOW_RADIO_FULLThe RPWI In-situ_slow + Radio_Full mode: - Makes continuous In-situ_slow mode measurement, the basic in-situ modes; - Makes detailed radio emissions from Jupiter as well as moons (Ganymede, Callisto, Europa). Will also support RIME measurements, giving the background natural radio emissions. Monitor the radio emission spectrum as well as polarization.RPWI
RPW_In_situ_slow_Radar_mode_3The RPWI In-situ_slow + Radio_mode_3 mode: - Makes continuous In-situ_slow mode measurement, the basic in-situ modes; - Radio mode TBDRPWI
MAJ_JUP_LIMB_SLEWThe scan the atmosphere of Jupiter over the limb up to 3000k is performed with a specific slew of the S/C Individual lines are largely overlapped to provide actual supersampling (x 10) in the spatial domain and allow sub-pixel resolution by deconvolution. Typically, we have cubes of about 300 lines by 50 pixels (~7500 km) Pointing type: OFF-NADIR (nominal pointing position over the Jupiter limb), continuous tracking (‘track tangent limb’) satellite orientation:LIMB TANGENT (MAJIS slit tangent to the limb), very slow s/c slew to get oversampling (10 lines corresponding to one pixel IFOV) Duration: 55 min for each cube (300 lines)MAJIS
SWI_2D_MAP_PS_V1This is a multi-purpose mode that can be used on any science target for any 2D mapping, and meridional or zonal rasters. This mode will also be used for calibration purposes (e.g. pointing). The number of rows and columns and the stepsize of the raster map is adaptable to the target angular size. Jupiter: Investigation of the global and regional stratospheric composition and temperature of Jupiter, and pointing calibration. For 2D maps, meridional scans and zonal scans, two CTS spectra are recorded for 60 seconds over 10000 channels (16 bits coding). Moon monitoring: Investigation of the spatial distribution of Galilean moons atmospheric species (+ monitoring), and calibration. Two CTS spectra are recorded for 60 seconds over 210 channels (16 bits coding). Flybys: Mapping of Galilean Moons’ surface properties and atmospheric composition, temperature, and winds. Two CTS spectra are recorded for 30 seconds over 210 channels (16 bits coding). GCO: (1) Investigation of Ganymede’s atmospheric composition, temperature, and winds, and surface properties by scanning from limb to limb with the along-track mechanism across the ground-track using the antenna mechanism ( 72 ). Two CTS spectra are recorded for 10 seconds over 130 channels (16 bits coding). (2) Tomographic investigation of Ganymede’s atmospheric and surface composition, temperature, and winds by scanning along-track from 30km to +30km of the nadir axis with 9 steps, using the rocker mechanism ( 4.3 ), and with 1.5 sec integration time for two CTS spectra over 130 channels (16 bits coding). In all cases, two CCH measurements (20 bits coding) are recorded for 0.1 second. During GCO, this implies that two CCH measurements are separated by 1/2 beam at 1200 GHz. Position-switch calibration method (the OFF position is observed after each ON of the map is observed).SWI
MAG_DLThis observation is introduced to characterize JMAG operations during downlink times where power resources from the SC may be more limited, and where SC attitude is driven by operational constraints. Only MAGOBS and MAGIBS are operating.JMAG
MAG_DL_FOB_LIGHT_ONLYThis observation is introduced to characterise JMAG operations during downlink times where power resources from the SC may be more limited, and where SC attitude is driven by operational constraints In this particular observation FOB fluxgate is powered on with FSC as light-only.JMAG
MAG_DL_FOBThis observation is introduced to characterise JMAG operations during downlink times where power resources from the SC may be more limited, and where SC attitude is driven by operational constraints Only MAGOBS is operating.JMAG
MAG_DL_LIGHT_ONLYThis observation is introduced to characterise JMAG operations during downlink times where power resources from the SC may be more limited, and where SC attitude is driven by operational constraints. In this particular observation FIB & FOB fluxgates powered on with FSC as light-only.JMAG
UVS_JUP_HP_FEATURE_SCANTo assess the evolution of discrete phenomena (e.g., H Ly-alpha bulge, plumes, auroral features,…) using the HP port and pixellist mode.UVS
MAJ_ICUTo monitor the radiometric performances of MAJIS using VISNIR and IR sources Specifically, there are several goals A) tracking the evolution of the actual levels (before subtracting for CDS) in the digital dynamics (0-65535 at 100 kHz, 0-4095 at 1 MHz). Such an evolution could lead to adjust an offset which can be selected by TC (4 settings) so as to avoid reaching digital saturation for the read image before analog saturation. B) tracking the evolution of the dark current and cosmetics (new hot / dead pixels) C) tracking the evolution of the overall photometric response as a function of the signal (needed for the pipeline) Pointing: MAJIS scan mirror oriented towards the ICU (8.5°) Satellite orientation: Deep space Duration: 10minMAJIS
GAL_IDLETransition from OFF to IDLE mode (and IDLE to OFF)GALA
3GM_USO_ONUSO is SWON and muted3GM
UVS_SAT_STELL_OCCUVS airglow port stares at a fixed RA and DEC as the satellite occults the star.UVS
UVS_SAT_SOL_OCCUVS solar port stares at Sun as the satellite occults it.UVS
SWI_WARMUPWarm-up mode.SWI

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