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Group
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
GANYMEDE_FLYBY_UVS Working Group 1
CALLISTO_FLYBY_RIME_AJSCallisto active radar opportunity, anti-jovian sideWorking Group 1
CALLISTO_FLYBY_RIME_JSCallisto active radar opportunity, jovian sideWorking Group 1
CALLISTO_RPWI_PASSIVRADCallisto passive radar opportunity for RPWIWorking Group 1
EUROPA_FLYBY_RIME_AJSEuropa active radar opportunity, anti-jovian sideWorking Group 1
EUROPA_FLYBY_RIME_JSEuropa active radar opportunity, jovian sideWorking Group 1
EUROPA_RPWI_PASSIVRADEuropa passive radar opportunity for RPWIWorking Group 1
GANYMEDE_FLYBY_RIME_AJSGanymede active radar opportunity, anti-jovian sideWorking Group 1
GANYMEDE_FLYBY_RIME_JSGanymede active radar opportunity, jovian sideWorking Group 1
GANYMEDE_RPWI_PASSIVRADGanymede passive radar opportunity for RPWIWorking Group 1
ASTRO_IRR_ELARA Working Group 2
ASTRO_IRR2_SINOPE Working Group 2
CALLISTO_DISTANT Working Group 2
CALLISTO_FLYBY_WG2 Working Group 2
CHARACTERIZATION_IRR2_CARME Working Group 2
EUROPA_DISTANT Working Group 2
EUROPA_FLYBY_WG2 Working Group 2
GANYMEDE_DISTANT Working Group 2
GANYMEDE_FLYBY_WG2 Working Group 2
RING_PHASECURV_100 Working Group 2
RING_PHASECURV_110 Working Group 2
RING_PHASECURV_120 Working Group 2
RING_PHASECURV_130 Working Group 2
RING_PHASECURV_140 Working Group 2
RING_PHASECURV_150 Working Group 2
RING_PHASECURV_160 Working Group 2
RING_PHASECURV_170 Working Group 2
RING_PHASECURV_20 Working Group 2
RING_PHASECURV_30 Working Group 2
RING_PHASECURV_40 Working Group 2
RING_PHASECURV_50 Working Group 2
RING_PHASECURV_60 Working Group 2
RING_PHASECURV_70 Working Group 2
RING_PHASECURV_80 Working Group 2
RING_PHASECURV_90 Working Group 2
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
ASTRO_INNERAstrometry inner moonsWorking Group 2
ASTRO_IRR2_ANANKEAstrometry irregular moon AnankeWorking Group 2
ASTRO_IRR2_CARMEAstrometry irregular moon CarmeWorking Group 2
ASTRO_IRR1_CARPOAstrometry irregular moon CARPOWorking Group 2
ASTRO_IRR1_CHALDENEAstrometry irregular moon CHALDENEWorking Group 2
ASTRO_IRR1_HIMALIAAstrometry irregular moon HIMALIAWorking Group 2
ASTRO_IRR1_KALLICHOREAstrometry irregular moon KALLICHOREWorking Group 2
ASTRO_IRR1_LEDAAstrometry irregular moon LEDAWorking Group 2
ASTRO_IRR1_LYSITHEAAstrometry irregular moon LYSITHEAWorking Group 2
ASTRO_IRR1_TAYGETEAstrometry irregular moon TAYGETEWorking Group 2
ASTRO_IRR1_THEMISTOAstrometry irregular moon THEMISTOWorking Group 2
ASTRO_IRR2_PASIPHAEastrometry measurement with inertial pointing to moon PasiphaeWorking Group 2
CALLISTO_FB_RSCallisto Flyby remote sensingWorking Group 2
CHARACTERIZATION_IRR2_ANANKECharacterization irregular moon ANANKEWorking Group 2
CHARACTERIZATION_IRR_ELARACharacterization irregular moon ElaraWorking Group 2
CHARACTERIZATION_IRR2_PASIPHAEcharacterization irregular moon PasiphaeWorking Group 2
CHARACTERIZATION_IRR2_SINOPECharacterization irregular moon SinopeWorking Group 2
CHAR_IRR1Characterization irregular moons group 1 (see list below)Working Group 2
EUROPA_FB_RSEuropa Flyby remote sensingWorking Group 2
GANYMEDE_FB_RSGanymede flyby remote sensingWorking Group 2
IO_ECLIPSEIo observation while Io is in eclipse.Working Group 2
IO_TOR_DUSTIo torus dustWorking Group 2
IO_MAJ_COMPOSITIONIO_MAJ_COMPOSITIONWorking Group 2
IO_MAJ_HOTSPOTSIO_MAJ_HOTSPOTSWorking 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
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_HPRing high phaseWorking Group 2
RING_LPRing low phaseWorking 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
HIGHPHPROFILErings high phase profile (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
RINGSPIRAL_HPRINGSPIRAL_HP (high phase, Janus def)Working Group 2
RINGSPIRAL_MPRINGSPIRAL_MP (medium phase: JANUS Def)Working Group 2
ROI_INTERSECTIONROI_INTERSECTIONWorking Group 2
508_PasTest opportunity segment PasiphaeWorking Group 2
CALLISTO_FLYBY_RPWI_IONO_AJS Working Group 3
EUROPA_FLYBY_RPWI_IONO_AJS Working Group 3
GANYMEDE_FLYBY_RPWI_IONO_AJS Working Group 3
CALLISTO_IONOCALLISTO_IONO In situ Callisto ionosphere observationWorking Group 3
EUROPA_IONO_ISEUROPA_IONO_IS In situ Europa ionosphere observationWorking Group 3
CALLISTO_ENAFar approach energetic neutral atom imaging of CallistoWorking Group 3
EUROPA_ENAFar approach energetic neutral atom imaging of EuropaWorking Group 3
GANYMEDE_ENAFar approach energetic neutral atom imaging of GanymedeWorking Group 3
GANYMEDE_IONOGANYMEDE_IONO In situ Ganymede ionosphere 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
CALLISTO_WAKEIn situ Callisto wake observationWorking Group 3
EUROPA_TOR_ISIn situ Europa torus observationWorking Group 3
EUROPA_WAKEIn situ Europa wake observationWorking Group 3
GANYMEDE_WAKEIn situ Ganymede wake observationWorking Group 3

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