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Information about the RPW electrical antennas 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

Description of the operation

Context and objectives

The main objective is to acquiring RPW data during the electrical antennas (ANT) deployement (x3).

The antenna deployment will occure during the LEOP phase.

RPW will be switched-off before and after the antenna deployement.

The SSMM will be available.

MOC will control the deployment of the antennas.

The ANT deployement will be performed one by one, starting with the PZ (ANT1), then PY (ANT2), finally MY (ANT3). The deployment of the ANT1 will start at T1=TBD, the deployment of the ANT2 at T2=TBD, and the deployement of the ANT3 at T3=TBD. The details of the deployment is given in the RPW Antenna User Manual.

Operation timeline and instrument configuration overview


                                                           Fig. 1. Antenna's operation timeline


In this phase, RPW measures the noise of the platform. RPW is set in a single specific configuration for antenna deployment. Measurements will be also taken during the first and last 10 minutes before and after the antenna 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.

RPW is set in a specific configuration for ANT deployment. Measurements will be taken during the first and last 10 minutes (before and after the ANT deployment). RPW in BURST mode with both spectral modes (all frequencies for B) and waveforms.

Minimal requirements:

  • THR: B field on channel 1 and E on channel 2 (all frequencies, max freq resolution).
  • LFR: spectral mode for B and E at the maximum frequency resolution, waveforms at the minimum resolution
  • TDS snapshots at the minimum resolution

Maximal requirements

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

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 Antenna mode/configuration0 min
Antenna deployment data acquistion and visualizationBBeginning of the first Antenna deployment10 min
Antenna deployment data acquistion and visualizationCEnd of the third antenna deployment10+TBD min
Instrument switch offDRPW switch off20+TBD min

The table below gives the RPW modes and configurations (i.e., states) expected over the operation timeline.

First step

Last step

RPW configuration

Duration

Comment

ABRPW_NECP_ANT-DEPLOY_CONFIG110 min
BCRPW_NECP_ANT-DEPLOY_CONFIG2TBDDuration of ANT deployement (TBD)
CDRPW_NECP_ANT-DEPLOY_CONFIG110 min


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

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