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THEMIS-SCM THM – SCM – CDR – 08-April-2004 in Velizy

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Presentation on theme: "THEMIS-SCM THM – SCM – CDR – 08-April-2004 in Velizy"— Presentation transcript:

1 THEMIS-SCM THM – SCM – CDR – 08-April-2004 in Velizy
Test and Calibration Plan I&T Plans prior to shipment to UCB EGSE Design I&T and Spacecraft Integration Plans Implementation Schedule Bertrand delaPorte THM-SCM-CDR –

2 THEMIS-SCM SCM VERIFICATION – TEST MATRIX
I/f model EM FM1 to FM6 PA SC SC+PA Electrical Verification X Full Calibration Thermal Test Metrology (i/f, mass, CoG) (1) Vibration QUALIF Therm Vac QUALIF Vibration ACCEPT Pre-Integration IDPU Integration in spacecraft (1) : is the M.o.I. requested ? Bertrand delaPorte THM-SCM-CDR –

3 THEMIS-SCM I&T plans prior to delivery – SCM – SC (Sensor)
After winding of the internal tube Impedance verification done After potting of the magnetic core Magnetic flux response, with PA After overall potting soon After 3 axis assembly, with associated PA Transfer function, SC in mm-box Metrology, Vibrations Temperature limits Full Calibration in Chambon After delivery to UCB Thermal vacuum (EM only ?) Bertrand delaPorte THM-SCM-CDR –

4 Electrical verification After cubes assembly and potting
THEMIS-SCM I&T plans prior to delivery – SCM – PA 3D+ cubes Single flex Electrical verification Offset adjustment done After cubes assembly and potting Temperature test ( ) Bertrand delaPorte THM-SCM-CDR –

5 THEMIS-SCM I&T plans prior to delivery – SCM – full PA
After PCB cabling Electrical verification soon After assembly in the housing Metrology, Vibrations Full range Temperature Test With associated SC Transfer function, SC in mm-box Full Calibration in Chambon After delivery to UCB Thermal vacuum (EM only ?) Bertrand delaPorte THM-SCM-CDR –

6 THEMIS-SCM SCM - EGSE For Bench Test :
mu-metal box (to put the sensor inside) – one only ? EGSE Interface Box (to be plugged to the PA) Power Supply +/-10V, Signal Generator, Oscilloscope, multimeters For Integration in the spacecraft mu-metal box Signal Generator Portable PC + dedicated software, to be connected to the Themis acquisition system (in a LAN or via Internet) Bertrand delaPorte THM-SCM-CDR –

7 THEMIS-SCM SCM Bench Test Configuration Bertrand delaPorte
THM-SCM-CDR –

8 THEMIS-SCM MAGNETIC CALIBRATION STATION – CHAMBON LA FORET
Bertrand delaPorte THM-SCM-CDR –

9 THEMIS-SCM I&T AND SPACECRAFT INTEGRATION PLAN
Pre-intégration SCM – IDPU (DFB) Integration to the spacecraft Bertrand delaPorte THM-SCM-CDR –

10 THEMIS-SCM Pre-Integration with IDPU
I&T AND SPACECRAFT INTEGRATION PLAN Pre-Integration with IDPU An « Interface Model » of the Pre-Amp will be provided for that purpose Same Power, Command, analog output interfaces Power and Cal Mode identification by led Cal Signal re-injected to the input A signal generator can be connected to each input Validation can only be done by analysis of the telemetry data (tbd) Bertrand delaPorte THM-SCM-CDR –

11 THEMIS-SCM Integration in the spacecraft
I&T AND SPACECRAFT INTEGRATION PLAN Integration in the spacecraft Delivery (Incoming Inspection, Bench Test) Mechanical Integration of the PA, connection to the boom harness Sensor in the mu-metal box, connection to the boom harness Electrical Integration (bounding, isolation, dangerous voltage) Power ON and functionnal Test Validation can only be done by analysis of the telemetry data (tbd) Bertrand delaPorte THM-SCM-CDR –

12 THEMIS-SCM SCM – INTEGRATION IN THE SPACECRAFT Initial configuration
The sensor is inside the mu-metal box, connected to the PA via the boom harness Requirement: to keep the sensor in the mu-metal box until all experiments are integrated in the spacecraft (mission operation test) Question: what is performed in UCB, and what is done in Swales ? Bertrand delaPorte THM-SCM-CDR –

13 THEMIS-SCM SCM Mu-metal box Bertrand delaPorte
THM-SCM-CDR –

14 THEMIS-SCM SCM – INTEGRATION IN THE SPACECRAFT
WHAT CAN BE DONE WITH THE SENSOR IN THE MU-METAL BOX axis identification re-verification of the end-to-end calibration Phase relation within the 3 components (for the waveforms) check of the conducted noise SCM/EField timing reference [and inter-calibration] (tbd) Bertrand delaPorte THM-SCM-CDR –

15 THEMIS-SCM SCM – INTEGRATION IN THE SPACECRAFT
SENSOR MOUNTED ON THE BOOM PA saturated by the 50/60 Hz except in a quite site (i.e. Chambon), or in an EMC chamber No measurement possible but a big failure would be seen INSTALLATION OF THE MLI - by UCB when ? Bertrand delaPorte THM-SCM-CDR –

16 THEMIS-SCM SCM – INTEGRATION – QUICK TESTS WITH HOUSEKEEPING
A few Housekeeping are needed to check the experiment rapidly (if possible in real time) during the ground tests and in the commissioning. HOUSEKEEPING FOR SCM: SCM-PWR-STATUS ( 1 bit ) SCM-CAL-STATUS ( 1 bit ) SCM-VOLT-MONITOR ( 8 bits ) SCM-MEAN-VAL-BX, __BY, __BZ ( 16 or 8 bits ) Mean average of |Bi| over one TM format (similar to r.m.s. value) Bertrand delaPorte THM-SCM-PDR –

17 THEMIS-SCM AC MAGNETIC NOISE VERIFICATION
In the low frequency range (< 4 kHz), the main sources of AC noise are The beating within several higher frequencies, especially the DC/DC Converters if they are not synchronised. It can be conducted and/or radiated. The solar pannels (cannot be verified on the ground) The CETP can help to analyse the AC radiated noise around the spacecraft. A « magnetic sniffer » has been designed and built for that purpose. In order to avoid the saturation by the 50/60 Hz, the analysis is separated into two bandwidths: below 50 Hz and above 300 Hz (5th harmonic) Bertrand delaPorte THM-SCM-CDR –

18 THEMIS-SCM SCM INTEGRATION – TEAM SUPPORT
The SCM team will support all critical activities of the integrations. However, due to the large number of satellites, a strategy must be imagined to limit the number of travels, the cost and the time spent The EM integration will be supported The FM will be delivered 3 by 3 and the level of support for each test will be agreed with UCB Capability of remote supporting should be implemented Bertrand delaPorte THM-SCM-CDR –

19 THEMIS-SCM EXAMPLE OF REAL TIME SUPPORT Bertrand delaPorte
THM-SCM-CDR –

20 THEMIS-SCM SCM SCHEDULE – KEY DATES EM delivery to UCB for TV
31-May-2004 EM available for integration in UCB 11-Jun-2004 FM 3D cubes delivered to CETP 23-Jul-2004 FM-1,2,3 available (without TV) 24-Sep-2004 FM-4,5,6 available (without TV) 10-Nov-2004 Bertrand delaPorte THM-SCM-CDR –

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23 THEMIS-SCM Bertrand delaPorte THM-SCM-CDR –


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