SOC_RIDER_OBSERVATION | Placeholder for SOC Rider Observation | SOC |
SOC_DESIGNER_OBSERVATION | | SOC |
NAVCAM_RIDER_OBSERVATION | Placeholder Segment to accomodate the detailed scenario observation plan generation process. | NAVCAM |
NAVCAM_DESIGNER_OBSERVATION | | NAVCAM |
RADEM_RIDER_OBSERVATION | | RADEM |
RADEM_DESIGNER_OBSERVATION | | RADEM |
GALA_RIDER_OBSERVATION | Placeholder for JUICE SOC Observations. | GALA |
GALA_DESIGNER_OBSERVATION | | GALA |
3GM_RIDER_OBSERVATION | Placeholder Segment to accomodate the detailed scenario observation plan generation process. | 3GM |
3GM_DESIGNER_OBSERVATION | | 3GM |
RPWI_RIDER_OBSERVATION | Placeholder Segment to accomodate the detailed scenario observation plan generation process. | RPWI |
JMAG_RIDER_OBSERVATION | Placeholder Segment to accomodate the detailed scenario observation plan generation process. | JMAG |
JMAG_DESIGNER_OBSERVATION | | JMAG |
SWI_RIDER_OBSERVATION | | SWI |
SWI_DESIGNER_OBSERVATION | | SWI |
RIME_RIDER_OBSERVATION | | RIME |
RIME_DESIGNER_OBSERVATION | | RIME |
UVS_RIDER_OBSERVATION | Placeholder Segment to accomodate the detailed scenario observation plan generation process. | UVS |
UVS_DESIGNER_OBSERVATION | | UVS |
MAJIS_RIDER_OBSERVATION | Placeholder Segment to accomodate the detailed scenario observation plan generation process. | MAJIS |
MAJIS_DESIGNER_OBSERVATION | | MAJIS |
JANUS_RIDER_OBSERVATION | Placeholder for JUICE SOC Observations. | JANUS |
JANUS_DESIGNER_OBSERVATION | | JANUS |
EUR_CAL_GAN_TRANSIT_PR | Triple transit in front of Jupiter | WGX |
GAN_CAL_TRANSIT_PR | Double transit in front of Jupiter (Ganymede, Callisto) | WGX |
GAN_EUR_TRANSIT_PR | Double transit in front of Jupiter (Europa, Ganymede) | WGX |
EUR_CAL_TRANSIT_PR | Double transit in front of Jupiter (Europa, Callisto) | WGX |
JMAG_CALROLL | 5 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 GOI | WGX |
FB_BATTERY_RECOVERY_STANDARD | Segment to allow for battery recharge | GENERIC |
FB_BATTERY_RECOVERY_FAST | Segment to allow for battery recharge | GENERIC |
JUPITER_FD_WOL_FB | In 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_FD_WOL | Flight dynamics wheel off-loading slot, outside of Flyby preparation and recuperation | GENERIC |
FB_THERMAL | FB_THERMAL | GENERIC |
TRANSIT_ET | Event tool support segment definition | GENERIC |
SUN_OCC_ET | Event tool support segment definition | GENERIC |
STELLAR_OCC_ET | Event tool support segment definition | GENERIC |
FLYBY_ET | Event tool support segment definition | GENERIC |
EARTH_OCC_ET | Event tool support segment definition | GENERIC |
ECLIPSE_JUPITER_THERMAL | ECLIPSE_JUPITER_THERMAL | GENERIC |
TRAJECTORY_SEGMENT | defined segment for moon coverage tool export functionnality | GENERIC |
DEFAULT_THERMAL | DEFAULT_THERMAL | GENERIC |
ECLIPSE_BATTERY_RECOVERY_STANDARD | Battery recharge after eclipse | GENERIC |
ECLIPSE_BATTERY_RECOVERY_FAST | Battery recharge after eclipse | GENERIC |
STELLAR_UVS_OCC_ET | | GENERIC |
SPICE_ATT_GOTOMARS_NPO | | GENERIC |
SPICE_ATT_GOTOMARS_NOA_HOT | | GENERIC |
SPICE_ATT_GOTOGANYMEDE_PHASE_SUP_SOL_CONJ | | GENERIC |
SPICE_ATT_GOTOGANYMEDE_NPO | | GENERIC |
SPICE_ATT_GOTOGANYMEDE_NOA_HOT | | GENERIC |
SPICE_ATT_GOTOGANYMEDE_NOA | | GENERIC |
SPICE_ATT_GOTOEUROPA_NPO | | GENERIC |
SPICE_ATT_GOTOEUROPA_NOA_HOT | | GENERIC |
SPICE_ATT_GOTOEUROPA_NOA | | GENERIC |
SPICE_ATT_GOTOEARTH_NPO | | GENERIC |
SPICE_ATT_GOTOEARTH_NOA_HOT | | GENERIC |
SPICE_ATT_GOTOEARTH_NOA | | GENERIC |
SPICE_ATT_GOTOCALLISTO_NPO | | GENERIC |
SPICE_ATT_GOTOCALLISTO_NOA_HOT | | GENERIC |
SPICE_ATT_GOTOCALLISTO_NOA | | GENERIC |
RECOVERY | | GENERIC |
JUPITER_FD_TCM | | GENERIC |
JUPITER_FD_NAV_FB | | GENERIC |
JUPITER_FD_EPHEM_GAN | | GENERIC |
JUPITER_FD_EPHEM_EUR | | GENERIC |
JUPITER_FD_EPHEM_CAL | | GENERIC |
SUN_OCC | Solar occultation by Jupiter, as seen from the SC. | Working Group 4 |
JUPITER_PERIJOVE | Jupiter observations | Working Group 4 |
EARTH_OCC_INGRESS | Earth occultation by Jupiter. Ingress | Working Group 4 |
EARTH_OCC_EGRESS | Earth occultation by Jupiter. Egress | Working Group 4 |
PERIJOVE_TERMINATOR | | Working Group 4 |
PERIJOVE_NIGHTSIDE | | Working Group 4 |
PERIJOVE_DAYSIDE | | Working Group 4 |
JUPITER_PHASE_MIN | | Working Group 4 |
JUPITER_PHASE_MAX | | Working Group 4 |
JUPITER_PHASE_165_INC | | Working Group 4 |
JUPITER_PHASE_165_DEC | | Working Group 4 |
JUPITER_PHASE_150_INC | | Working Group 4 |
JUPITER_PHASE_150_DEC | | Working Group 4 |
JUPITER_PHASE_135_INC | | Working Group 4 |
JUPITER_PHASE_135_DEC | | Working Group 4 |
JUPITER_PHASE_120_INC | | Working Group 4 |
JUPITER_PHASE_120_DEC | | Working Group 4 |
JUPITER_PHASE_090 | | Working Group 4 |
JUPITER_MONITORING | | Working Group 4 |
JUPITER_INCLINED_AURORA | | Working Group 4 |
INCLINED_SOUTH | | Working Group 4 |
INCLINED_NORTH | | Working Group 4 |
JUPITER_TAIL | In situ search for signatures of local magnetic reconnection in the Jovian magnetotail | Working Group 3 |
JUPITER_GM | In 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_GM | In situ mapping of global configuration and monitoring dynamics of Ganymede's magnetospheric environment | Working Group 3 |
JUPITER_PDT | In situ Jupiter particle distribution transition region observation.
Maximize pitch angle coverage for PEP/JEI, JDC,JoEE, JENI (ion mode) | Working Group 3 |
JUPITER_NULL | In situ Jupiter magnetic null search | Working Group 3 |
JUPITER_CPS | In situ Jupiter current/plasma sheet observation | Working Group 3 |
JUPITER_CB | In 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_CP | In 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.
CP stands for corotation profile | Working Group 3 |
GANYMEDE_WAKE | In situ Ganymede wake observation | Working Group 3 |
EUROPA_WAKE | In situ Europa wake observation | Working Group 3 |
EUROPA_TOR_IS | In situ Europa torus observation | Working Group 3 |
CALLISTO_WAKE | In situ Callisto wake observation | Working Group 3 |
JUPITER_ENA | Imaging 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 torus | Working Group 3 |