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Information about the I-Boom deployment operation during the LEOP.


Working Group Members

RPW sub-system teams will also contribute to define the RPW modes to be set during the deployement.

Contact at MOC

  • Sylvain dot Lodiot at esa dot int

Operation timeline and instrument configuration overview
















Fig. 1. I-Boom operation timeline


In this phase, RPW measures the noise of the platform. RPW is set in a single specific configuration for I-BOOM deployment. Measurements will be also taken during the first and last 10 minutes before and after the IBOOM deployment. RPW in SURVEY_BURST SCIENCE submode with both spectral modes (all frequencies for B) and waveforms. The instrument is expected to be switched off before and after the operation.

Minimal requirements:

  • THR: B field on channel 1 and E on channel 2 (all frequencies, max freq resolution).
  • LFR: spectral mode maximum frequency resolution.
  • No TDS.

Maximal requirements

  • THR: B field on channel 1 and E on channel 2 (all frequencies).
  • LFR: spectral mode maximum frequency resolution, B waveforms at 256 Hz.
  • TDS snapshots

The table below gives the organization of the operation stages and associated timing.

Activity

Step

Description

Time since beginning

Instrument initializationARPW switch on and go to I-BOOM mode/configuration0 min
I-BOOM deployment data acquistion and visualizationBBeginning of the I-BOOM deployment10 min
I-BOOM deployment data acquistion and visualizationCEnd of the I-BOOM deployment130 min
Instrument switch offDRPW switch off140 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

ADRPW_NECP_IBOOM-DEPLOY_CONFIG1140 min.A single configuration will be used during the entire operation timeline.

Orbitography

TBW

Success criteria

TBW

Operational constraints, assumptions and dependencies

Resources allocation

Power consumption allocation

TBW

Telemetry allocation

900 kbps available for platform + payload.

Details of allocation are TBD

Instrument-related constraints, assumptions and dependencies

The DPU SCIENCE SBM_DETECTION submode can be applied on-board during NECP, but there is not guarantee that the resulting SBM data stored on the SSMM can be downlinked to ground by MOC during this phase. (Note that the dump of the SBM data by the DPU can be forced by TC, since in the nominal case the transfer of data from the DPU SBM buffers to the SSMM is only done when an event is detected on-board.)

Spacecraft-related constraints, assumptions and dependencies

TBW

Ground constraints, assumptions and dependencies

TBW

Related resources

Meeting Notes

Actions Items

Key Summary T Created Updated Due Assignee Reporter P Status Resolution
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