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DL_Downlink communication prime segments. pointing: HGA pointing to EarthGENERIC
E_GPH_7E1E_GPH_7E1Working Group 1
E_GPH_8E2E_GPH_8E2Working Group 1
E_IS_OBSE_IS_OBSWorking Group 3
E_RS_7E1E_RS_7E1Working Group 2
E_RS_8E2E_RS_8E2Working Group 2
SPICE_ATT_GOTOEARTH_COMMSEarth communication segmentGENERIC
EARTH_OCCEarth occultation by JupiterWorking Group 4
EARTH_OCC_EGRESSEarth occultation by Jupiter. EgressWorking Group 4
EARTH_OCC_INGRESSEarth occultation by Jupiter. IngressWorking Group 4
ECLIPSE_JUPITER_THERMALECLIPSE_JUPITER_THERMALGENERIC
EUROPA_FLYBY_RIME_AJSEuropa active radar opportunity, anti-jovian sideWorking Group 1
EUROPA_FLYBY_RIME_JSEuropa active radar opportunity, jovian sideWorking Group 1
EUROPA_FB_RSEuropa Flyby remote sensingWorking Group 2
E_GPH_OBSEuropa geophysics generic containing obs database linkWorking Group 1
EUROPA_RPWI_PASSIVRADEuropa passive radar opportunity for RPWIWorking Group 1
E_RS_OBSEuropa remote sensing generic segment containing obs database linkWorking Group 2
EUROPA_IONO_ISEUROPA_IONO_IS In situ Europa ionosphere observationWorking Group 3
EARTH_OCC_ETEvent tool support segment definitionGENERIC
FLYBY_ETEvent tool support segment definitionGENERIC
STELLAR_OCC_ETEvent tool support segment definitionGENERIC
SUN_OCC_ETEvent tool support segment definitionGENERIC
TRANSIT_ETEvent tool support segment definitionGENERIC
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
FB_THERMALFB_THERMALGENERIC
JUPITER_FD_WOLFlight dynamics wheel off-loading slot, outside of Flyby preparation and recuperationGENERIC
G_GPH_26G6G_GPH_26G6Working Group 1
G_GPH_3G3G_GPH_3G3Working Group 1
G_GPH_5G5G_GPH_5G5Working Group 1
G_IS_OBSG_IS_OBSWorking Group 3
G_RS_OBSG_RS GENERICWorking Group 2
G_RS_26G6G_RS_26G6Working Group 2
G_RS_27G7G_RS_27G7Working Group 2
G_RS_30G8G_RS_30G8Working Group 2
G_RS_32G9G_RS_32G9Working Group 2
G_RS_33G10G_RS_33G10Working Group 2
G_RS_34G11G_RS_34G11Working Group 2
G_RS_35G12G_RS_35G12Working Group 2
GANYMEDE_FLYBY_RIME_AJSGanymede active radar opportunity, anti-jovian sideWorking Group 1
GANYMEDE_FLYBY_RIME_JSGanymede active radar opportunity, jovian sideWorking Group 1
GANYMEDE_FB_RSGanymede flyby remote sensingWorking Group 2
G_IS_3G3Ganymede in-situ observations around closest approachWorking Group 3
GANYMEDE_RPWI_PASSIVRADGanymede passive radar opportunity for RPWIWorking Group 1
GANYMEDE_IONOGANYMEDE_IONO In situ Ganymede ionosphere observationWorking Group 3
G_GPH_OBSGeneric G_GPH containing link to obs defWorking Group 1
G_RS_3G3HAA as per 3GM UM IS considering NIMWorking Group 2
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
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
JUPITER_CPSIn situ Jupiter current/plasma sheet observationWorking Group 3
JUPITER_NULLIn situ Jupiter magnetic null searchWorking 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
GANYMEDE_GMIn situ mapping of global configuration and monitoring dynamics of Ganymede's magnetospheric environmentWorking 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
JUPITER_TAILIn situ search for signatures of local magnetic reconnection in the Jovian magnetotailWorking Group 3
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
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
J_SAT_505_AmaJ_SAT_505_AmaWorking Group 2
J_SAT_514_TheJ_SAT_514_TheWorking Group 2
J_SAT_515_AdrJ_SAT_515_AdrWorking Group 2
J_SAT_516_MetJ_SAT_516_MetWorking Group 2
J_SAT_55507_3J23J_SAT_55507_3J23Working Group 2
J_SAT_OBSJ_SAT_OBSWorking Group 2
JA_PE_OBSJA_PE generic for link obs<-> segmentsWorking Group 4
JA_PE21JA_PE21Working Group 4
JA_PE25JA_PE25Working Group 4
JA_PE60JA_PE60Working Group 4
JA_PE61JA_PE61Working Group 4
JA_PE62JA_PE62Working Group 4
JA_PE63JA_PE63Working Group 4
JA_PE64JA_PE64Working Group 4
JA_PE65JA_PE65Working Group 4
JA_PE66JA_PE66Working Group 4
JA_PE67JA_PE67Working Group 4
JA_PE68JA_PE68Working Group 4
JA_PE69JA_PE69Working Group 4
JA_INCLJupiter Atmosphere Inclined segments: at maximum (Northern) and/or minimum (Southern) latitudes. Pointing target uis Jupiter although pointing details are TBD (track, limb etc...)Working Group 4
JA_MJupiter Atmosphere Monitoring segments: at regular interval during the tour. Pointing taregt is Jupiter, although pointing type is TBD (slew scan, raster, nadir etc)Working Group 4
JA_PE17Jupiter Atmosphere prime segment around perijove pass. Pointing target is Jupiter although pointing details are TBD (track, limb, nadir etc)Working Group 4
JA_PHJupiter Atmosphere prime segment at min-90-max phase. pointing target is Jupiter although pointing type is TBD (limb, etc)Working Group 4
JM_GMJupiter Magnetosphere global monitoring. Large pointing flexibility, constraints mainly driven by PEPWorking Group 3
JM_PE_OBSJupiter Magnetosphere perijove segments containing link to observations databaseWorking Group 3
JUPITER_PERIJOVEJupiter observationsWorking Group 4
J_SATjupiter satellite GENERICWorking Group 2
OPNAV_CALOPNAV_CAL Optical navigation window, targeting Callisto. Pointing is Callisto trackingGENERIC
OPNAV_EUROPNAV_EUR Optical navigation window, targeting Europa. Pointing is Europa tracking (MPAD)GENERIC
OPNAV_GANOPNAV_GAN Optical navigation window, targeting Ganymede. Pointing is Ganymede trackingGENERIC
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
RIME_OBSERVATIONPlaceholder Segment to accomodate the detailed scenario observation plan generation process.RIME
J_FD_WOLRegular Wheel off loading s Pointing is TBDGENERIC
RING_HPRing high phaseWorking Group 2

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