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EUR_CAL_GAN_TRANSIT_PRTriple transit in front of JupiterWGX
SUN_OCCSolar occultation by Jupiter, as seen from the SC.Working Group 4
ROI_INTERSECTIONROI_INTERSECTIONWorking Group 2
RINGSPIRAL_MPRINGSPIRAL_MP (medium phase: JANUS Def)Working Group 2
RINGSPIRAL_HPRINGSPIRAL_HP (high phase, Janus def)Working Group 2
SHADOWEDGErings SHADOWEDGE. Imaging of the ring region intersected by the planetary shadow at moderate elevation and very high phase. Especially for the very faint gossamer rings and the Thebe extensionWorking Group 2
HIGHPHPROFILErings high phase profile (JANUS DEF)Working Group 2
RINGMATTERRINGMATTER. Observations of the main rings and the gossamer rings, imaging the ring ansae from moderately large elevation. The moderatly large elevation will reveal azimuthal structure in the rings and the presence of clumps at the resolution limit of the imaging.Working Group 2
RING_LPRing low phaseWorking Group 2
RING_HPRing high phaseWorking Group 2
RING_PHASECURV_5Opportunity implementation in geopipeline SC distance to Jupiter larger than 8e5 km SC elevation above the rings lower than 0.5 deg Only one Ansae tested for phase conditions - value must be between 5 deg and 10 degWorking Group 2
RING_PHASECURV_10Opportunity implementation in geopipeline SC distance to Jupiter larger than 8e5 km SC elevation above the rings lower than 0.5 deg Only one Ansae tested for phase conditions - value must be between 10 deg and 20 degWorking Group 2
JUPITER_PERIJOVEJupiter observationsWorking Group 4
IO_MAJ_HOTSPOTSIO_MAJ_HOTSPOTSWorking Group 2
IO_MAJ_COMPOSITIONIO_MAJ_COMPOSITIONWorking Group 2
IO_TOR_DUSTIo torus dustWorking Group 2
IO_ECLIPSEIo observation while Io is in eclipse.Working Group 2
JUPITER_FD_WOL_FBIn the last week before the fly-by a WOL slot shall be combined with the TCM slot at To– 3 days (i.e. a single 3-hr slot). Another 2-hour WOL slot shall be reserved at To + 12 hours.GENERIC
JUPITER_TAILIn situ search for signatures of local magnetic reconnection in the Jovian magnetotailWorking Group 3
JUPITER_GMIn situ mapping of global configuration and monitoring dynamics of the Jovian magnetospheric environment. corotation should be in the FoV of PEP/JDC or PEP/JEI. Conditions for coverage: ◦ Minimum angle less than about 11.25 deg (half-azimuthal sector size) of a JEI or JDC pixel from corotation ◦ Boresight angle of JDC or JEI less than ˜90 deg Conditions for ideal coverage: ◦ Minimum angle less than about 11.25 deg (half-azimuthal sector size) of a JEI or JDC pixel from corotation ◦ Boresight angle less than ˜75 deg (JEI) or 70 deg (JDC): corotation away from the FoV edge JDC is preferred for monitoring corotation, over JEI, when possible.Working Group 3
GANYMEDE_GMIn situ mapping of global configuration and monitoring dynamics of Ganymede's magnetospheric environmentWorking Group 3
JUPITER_PDTIn situ Jupiter particle distribution transition region observation. Maximize pitch angle coverage for PEP/JEI, JDC,JoEE, JENI (ion mode)Working Group 3
JUPITER_NULLIn situ Jupiter magnetic null searchWorking Group 3
JUPITER_CPSIn situ Jupiter current/plasma sheet observationWorking Group 3
JUPITER_CBIn situ Jupiter corotation breakdown region and plasma transport observation. Maximize the intervals for which co-rotation is measured to build spatial and temporal coverage of corotation profiles across the magnetosphere and also in the local moon environments.Working Group 3
GANYMEDE_WAKEIn situ Ganymede wake observationWorking Group 3
EUROPA_WAKEIn situ Europa wake observationWorking Group 3
EUROPA_TOR_ISIn situ Europa torus observationWorking Group 3
CALLISTO_WAKEIn situ Callisto wake observationWorking Group 3
JUPITER_ENAImaging of Jupiter's magnetosphere in energetic neutral atoms (ENAs).Maximize pitch angle coverage with PEP JEI,JDC,JoEE, JENI (ion mode) a) JENI has a broad FoV and captures Jupiter and the Io/Europa torus and magnetosphere at most times. No special pointing design required for JENI besides requiring an approximate nadir pointing (considerable offsets can still be acceptable) b) JNA disk-shaped/slit FoV has a slight offset from the XZ spacecraft plane, meaning that during nadir pointing, it images preferentially the northern or southern extension of the Europa/Io torus, whereas Jupiter may be in the edge or outside of the FoV, especially at large distances. Scans (small rotations around Sc-X) or periods with stable, small offset of the SC-xz plane from Nadir can help to better image stronger emissions from the equatorial torusWorking Group 3
GANYMEDE_IONOGANYMEDE_IONO In situ Ganymede ionosphere observationWorking Group 3
GANYMEDE_RPWI_PASSIVRADGanymede passive radar opportunity for RPWIWorking Group 1
GANYMEDE_FB_RSGanymede flyby remote sensingWorking Group 2
GANYMEDE_FLYBY_RIME_JSGanymede active radar opportunity, jovian sideWorking Group 1
GANYMEDE_FLYBY_RIME_AJSGanymede active radar opportunity, anti-jovian sideWorking Group 1
JUPITER_FD_WOLFlight dynamics wheel off-loading slot, outside of Flyby preparation and recuperationGENERIC
FB_THERMALFB_THERMALGENERIC
GANYMEDE_ENAFar approach energetic neutral atom imaging of GanymedeWorking Group 3
EUROPA_ENAFar approach energetic neutral atom imaging of EuropaWorking Group 3
CALLISTO_ENAFar approach energetic neutral atom imaging of CallistoWorking Group 3
SUN_OCC_ETEvent tool support segment definitionGENERIC
FLYBY_ETEvent tool support segment definitionGENERIC
TRANSIT_ETEvent tool support segment definitionGENERIC
EARTH_OCC_ETEvent tool support segment definitionGENERIC
STELLAR_OCC_ETEvent tool support segment definitionGENERIC
EUROPA_IONO_ISEUROPA_IONO_IS In situ Europa ionosphere observationWorking Group 3
EUROPA_RPWI_PASSIVRADEuropa passive radar opportunity for RPWIWorking Group 1
EUROPA_FB_RSEuropa Flyby remote sensingWorking Group 2
EUROPA_FLYBY_RIME_JSEuropa active radar opportunity, jovian sideWorking Group 1
EUROPA_FLYBY_RIME_AJSEuropa active radar opportunity, anti-jovian sideWorking Group 1
ECLIPSE_JUPITER_THERMALECLIPSE_JUPITER_THERMALGENERIC
EARTH_OCC_INGRESSEarth occultation by Jupiter. IngressWorking Group 4
EARTH_OCC_EGRESSEarth occultation by Jupiter. EgressWorking Group 4
GAN_CAL_TRANSIT_PRDouble transit in front of Jupiter (Ganymede, Callisto)WGX
GAN_EUR_TRANSIT_PRDouble transit in front of Jupiter (Europa, Ganymede)WGX
EUR_CAL_TRANSIT_PRDouble transit in front of Jupiter (Europa, Callisto)WGX
TRAJECTORY_SEGMENTdefined segment for moon coverage tool export functionnalityGENERIC
DEFAULT_THERMALDEFAULT_THERMALGENERIC
CHAR_IRR1Characterization irregular moons group 1 (see list below)Working Group 2
CHARACTERIZATION_IRR2_SINOPECharacterization irregular moon SinopeWorking Group 2
CHARACTERIZATION_IRR2_PASIPHAEcharacterization irregular moon PasiphaeWorking Group 2
CHARACTERIZATION_IRR_ELARACharacterization irregular moon ElaraWorking Group 2
CHARACTERIZATION_IRR2_ANANKECharacterization irregular moon ANANKEWorking Group 2
CALLISTO_IONOCALLISTO_IONO In situ Callisto ionosphere observationWorking Group 3
CALLISTO_RPWI_PASSIVRADCallisto passive radar opportunity for RPWIWorking Group 1
CALLISTO_FB_RSCallisto Flyby remote sensingWorking Group 2
CALLISTO_FLYBY_RIME_JSCallisto active radar opportunity, jovian sideWorking Group 1
CALLISTO_FLYBY_RIME_AJSCallisto active radar opportunity, anti-jovian sideWorking Group 1
ASTRO_IRR2_PASIPHAEastrometry measurement with inertial pointing to moon Pasiphae Working Group 2
ASTRO_IRR1_THEMISTOAstrometry irregular moon THEMISTOWorking Group 2
ASTRO_IRR1_TAYGETEAstrometry irregular moon TAYGETEWorking Group 2
ASTRO_IRR1_LYSITHEAAstrometry irregular moon LYSITHEAWorking Group 2
ASTRO_IRR1_LEDAAstrometry irregular moon LEDAWorking Group 2
ASTRO_IRR1_KALLICHOREAstrometry irregular moon KALLICHOREWorking Group 2
ASTRO_IRR1_HIMALIAAstrometry irregular moon HIMALIAWorking Group 2
ASTRO_IRR1_CHALDENEAstrometry irregular moon CHALDENEWorking Group 2
ASTRO_IRR1_CARPOAstrometry irregular moon CARPOWorking Group 2
ASTRO_IRR2_CARMEAstrometry irregular moon CarmeWorking Group 2
ASTRO_IRR2_ANANKEAstrometry irregular moon AnankeWorking Group 2
ASTRO_INNERAstrometry inner moonsWorking Group 2
JMAG_CALROLL5 calibration roll needed by JMAG. 2 as soon as possible after JOI. 3 during phase 5: one at the start of phase 5, the last 2 as late as possible before GOIWGX
IO_MONITORING- JANUS minimum distance = 7.00e+05 km - MAJIS minimum distance = 8.00e+05 km - SWI minimum distance = 6.00e+05 km (able to resolve target when angular size is > 1 mrad) Working Group 2
GANYMEDE_FLYBY_UVS Working Group 1
CALLISTO_FLYBY Working Group 1
CALLISTO_FLYBY_3GM Working Group 1
CALLISTO_FLYBY_GALA Working Group 1
CALLISTO_FLYBY_JANUS Working Group 1
CALLISTO_FLYBY_MAJIS Working Group 1
EUROPA_FLYBY Working Group 1
EUROPA_FLYBY_3GM Working Group 1
EUROPA_FLYBY_GALA Working Group 1
EUROPA_FLYBY_JANUS Working Group 1
EUROPA_FLYBY_MAJIS Working Group 1
GANYMEDE_FLYBY Working Group 1
GANYMEDE_FLYBY_3GM Working Group 1
GANYMEDE_FLYBY_GALA Working Group 1
GANYMEDE_FLYBY_JANUS Working Group 1
GANYMEDE_FLYBY_MAJIS Working Group 1
RING_PHASECURV_170 Working Group 2
RING_PHASECURV_160 Working Group 2

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