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Group
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
EUR_CAL_TRANSIT_PRDouble transit in front of Jupiter (Europa, Callisto)WGX
GAN_EUR_TRANSIT_PRDouble transit in front of Jupiter (Europa, Ganymede)WGX
GAN_CAL_TRANSIT_PRDouble transit in front of Jupiter (Ganymede, Callisto)WGX
EUR_CAL_GAN_TRANSIT_PRTriple transit in front of JupiterWGX
JUPITER_FD_EPHEM_GAN GENERIC
JUPITER_FD_NAV_FB GENERIC
JUPITER_FD_TCM GENERIC
STELLAR_UVS_OCC_ET GENERIC
ECLIPSE_BATTERY_RECOVERY_FASTBattery recharge after eclipseGENERIC
ECLIPSE_BATTERY_RECOVERY_STANDARDBattery recharge after eclipseGENERIC
TRAJECTORY_SEGMENTdefined segment for moon coverage tool export functionnalityGENERIC
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
JUPITER_FD_WOLFlight dynamics wheel off-loading slot, outside of Flyby preparation and recuperationGENERIC
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
FB_BATTERY_RECOVERY_FASTSegment to allow for battery rechargeGENERIC
FB_BATTERY_RECOVERY_STANDARDSegment to allow for battery rechargeGENERIC
INCLINED_NORTH Working Group 4
INCLINED_SOUTH Working Group 4
JUPITER_INCLINED_AURORA Working Group 4
JUPITER_MONITORING Working Group 4
JUPITER_PHASE_090 Working Group 4
JUPITER_PHASE_120_DEC Working Group 4
JUPITER_PHASE_120_INC Working Group 4
JUPITER_PHASE_135_DEC Working Group 4
JUPITER_PHASE_135_INC Working Group 4
JUPITER_PHASE_150_DEC Working Group 4
JUPITER_PHASE_150_INC Working Group 4
JUPITER_PHASE_165_DEC Working Group 4
JUPITER_PHASE_165_INC Working Group 4
JUPITER_PHASE_MAX Working Group 4
JUPITER_PHASE_MIN Working Group 4
PERIJOVE_DAYSIDE Working Group 4
PERIJOVE_NIGHTSIDE Working Group 4
PERIJOVE_TERMINATOR Working Group 4
EARTH_OCC_EGRESSEarth occultation by Jupiter. EgressWorking Group 4
EARTH_OCC_INGRESSEarth occultation by Jupiter. IngressWorking Group 4
JUPITER_PERIJOVEJupiter observationsWorking Group 4
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
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
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

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