| SWI_ALLAN_TOTAL_CTS | Allan variance characterization of the CTS 1 & 2 by integrating on the cold
sky. Integration time is 1.5 s. | SWI |
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| SWI_ALLAN_TOTAL_CCH | Allan variance characterization of the CCH 1 & 2 by integrating on the cold sky. Integration time is 0.1 s. | SWI |
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| SWI_ALLAN_TOTAL_ACS | Allan variance characterization of the ACS 1 & 2 by integrating on the cold sky. Integration time is 1 s | SWI |
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| SWI_ALLAN_ACS_FS | Allan variance characterization of the ACS 1 & 2 by integrating on the cold
sky. Integration time is 1 s. Frequency-switch calibration method. | SWI |
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| PEP_JUPITER_EQUATORIAL_TORUS_CROSSING | All sensors, except JNA, on in medium to low rates. Prime objective is for NIM to measure torus composition in-situ. Other sensors to measure indicators that can be used to constrain the densities. Applies also to Jupiter High Inclination for now. | PEPLO |
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| PEL_OFF_1 | All sensors off, only survival heaters on
PEP-Lo off (e.g. TCM, WOL periods) | PEPLO |
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| SWI_OFF | All instrument subsystems including the DPU will be switched off. Consequently there will be no housekeeping data and no telemetry. The instrument will be in this mode during launch and cruise phase, except during calibration campaigns (e.g. planet flybys). | SWI |
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| MAJ_STANDBY | After switch-on of MAJIS, the Boot SW automatically starts, and performs the primary boot from the PROM (Init fugitive BSW mode).
After processor modules initialization, the Boot software goes to STANDBY mode. By default, the ASW Image0 (stored in MRAM0 = ASM0) is autonomously loaded after a timeout of 30 seconds. MAJIS then enters into ASW init Mode and then into SAFE mode.
In STANDBY Mode, all channels are off, and only DPU HK SID1 are received.
MAJIS needs to be maintained in STANDBY mode using the TC(17,1) in the following cases :
- upload (using service 6) of new ASW images (or CUSW, or firmware) into MRAM: FCP-MAJ-070 describes the maintenance process.
- upload a new BROWSE Table FCP-MAJ-060 into MRAM
- select ASW Image1 and then start ASW Image 1 instead of teh default ASW Image0. FCP-MAJ-062
- any other update of MRAM using service 6 | MAJIS |
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| MAJ_JUP_DISK_MOSAIC | A series of several MAJIS_JUP_DISK_SCAN or MAJIS_JUP_DISK_SLEW
Spacecraft has to be re-pointed between individual acquisitions.
POinting type: YS, NADIR with offset around Y (‘ nadir offset MAJIS scan’’)
satellite orientation: HORIZONTAL (preferred)
Duration:
3 x (scan-duration + turnaround Y duration). Scan duration from 20 to 40 min depending on the distance from Jupiter. Turnaround ~50 min | MAJIS |
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| PEH_JUPITER_IN_SITU_NOMINAL_1 | *Regular magnetosphere in-situ
monitoring mode
*Can work on flybys
* Macro: 117
Sensors ON: JENI, JoEE | PEPHI |
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| PEH_JUPITER_IN_SITU_IMAGING_BURST_1 | *Regular magnetosphere in-situ
& ENA imaging monitoring mode
* Macro: 148b
Sensors ON: JENI, JoEE. | PEPHI |
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| PEH_JUPITER_IN_SITU_LOW_1 | *Low power in-situ mode
(e.g. downlink, non-prime/low priority science sgments)
* Macro: 110
Sensors: JENI, JoEE | PEPHI |
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| PEH_JUPITER_IN_SITU_IMAGING_LOW_1 | *Low power in-situ & ENA imaging mode (e.g. downlink, non-prime/low priority science sgments
* Macro: 142
Sensors: JENI, JoEE | PEPHI |
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| PEH_JUPITER_IN_SITU_IMAGING_NOMINAL_1 | *Low power in-situ & ENA imaging mode (e.g. downlink, non-prime/low priority science sgments
* Macro: 142
Sensors ON: JENI, JoEE | PEPHI |
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| PEL_JUPITER_IN_SITU_IMAGING_BURST_2 | *Burst in-situ mode, magnetosphere
*CA of moon flybys with JNA/JENI imaging and high time (plume) resolution for NIM | PEPLO |
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| PEH_JUPITER_IN_SITU_BURST_1 | *Burst in-situ mode, magnetosphere
*CA of moon flybys
*Short duration events (magnetopause/bow shock crossings, injection events, moon wakes/microsignatures)
* Macro: 121
Sensors: JENI, JoEE | PEPHI |
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| PEH_GANYMEDE_IN_SITU_BURST_1 | *Burst in-situ mode, ganymede phase
*CA of moon flybys
*Short duration events (e.g. boundary crossings)
* Macro: 122 | PEPHI |
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| PEH_GANYMEDE_IN_SITU_NOMINAL_1 | * Regular in-situ mode, ganymede phase
*CA of moon flybys later in the mission (higher power consumption)
*Good for high quality, extended survey
* Macro: 118
Sensors: JENI, JoEE | PEPHI |
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| SWI_POINTING_ACS_CCH | : Determination of absolute pointing offset between S/C and SWI (for the 2 bands) recording continuum maps with the ACS 1 & 2 and the CCH 1 & 2.Integration time on the ACS and CCH are 1s and 0.1s, respectively. | SWI |
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| NAVCAM_DVOL_BLOCK | | JUICE |
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