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The table below gives the organization of the operation stages and associated timing.
Activity | Step | Description | Time since beginning |
|---|---|---|---|
| Instrument initialization | A | RPW switch on and go to I-BOOM mode/configuration | 0 min |
| I-BOOM deployment data acquistion and visualization | B | Beginning of the I-BOOM deployment | 10 min |
| I-BOOM deployment data acquistion and visualization | C | End of the I-BOOM deployment | 130 min |
| Instrument switch off | D | RPW switch off | 140 min |
The table below gives the RPW modes and configurations (i.e., states) expected for each step of the operation timeline.
First step | Last step | RPW configuration | Duration | Comment |
|---|---|---|---|---|
| A | D | RPW_NECP_IBOOM-DEPLOY_CONFIG1 | 140 min. | A single configuration will be used during the entire operation timeline. |
Orbitography
TBWN/A
Success criteria
TBWN/A
Operational constraints, assumptions and dependencies
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Power consumption allocation
TBWN/A
Telemetry allocation
900 kbps available for platform + payload.
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Spacecraft-related constraints, assumptions and dependencies
TBWN/A
Ground constraints, assumptions and dependencies
TBWN/A
Related resources
Meeting Notes
Open Actions Items
| Jira | ||||||||||
|---|---|---|---|---|---|---|---|---|---|---|
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- procedure_IBOOM_depl.docx
- RPW-related operations during LEOP – The SSMM will finally available during these operations.
- TDS configuration :
View file name RPW-2_TDS_inputs_iBoom_V02.docx height 250 - LFR configuration :
View file name RPW-2_LFR_inputs_V02.docx height 250