SOLAR ORBITER
SWA-PAS
COMMISSIONING LOG

CALIPSO 1 PAS FS rehearsal

The technical notes:

1.1 03 Mar 2020 Rehearsal of the first day of the commissioning:

The procedure and the data of the first commissioning day:
Table 1: Day one commissioning files
I have created two data bases of AMDA, see Figure 1. The conversion of the original EGSE files to the AMDA readable files is shown in Table 1
image: 0_home_fedorov_SOLARORB_PAS_FLIGHT_COMMISSIONING_DOCLOG_PAS_AMDA_params.jpg
Figure 1: AMDA parameters and files for Commissioning rehearsal
The Engineering scheme is shown in Figure 2. The same you can find in the PAS Bible.
image: 1_home_fedorov_SOLARORB_PAS_FLIGHT_COMMISSIONING_DOCLOG_Engineering_Steps_commis.jpg
Figure 2: Commissioning constants for Engineering steps
The performance is shown in Figure 3 and Figure 4
image: 2_home_fedorov_SOLARORB_PAS_FLIGHT_COMMISSIONING_DOCLOG_PAS_FS_comm_repet_day1_HV_03_Mar_2020.jpg
Figure 3: HK parameters during the Day1 of the commissioning rehearsal
image: 3_home_fedorov_SOLARORB_PAS_FLIGHT_COMMISSIONIN___PAS_FS_comm_repet_day1_TotCount_03_Mar_2020.jpg
Figure 4: Total count (top panel) during the Day1 of commissioning rehearsal
To compare the FS repetition and EQM repetition: Figure 5 shows the Day One HKs taken with the real flight procedure with EQM and SolO simulator at MSSL on 23 Dec 2019.
Note: the duration of the Engineering mode at MSSL procedure was 23 min. The real duration of the Engineering mode is exactly 20 min.
image: 4_home_fedorov_SOLARORB_PAS_FLIGHT_COMMISSIONING_DOCLOG_PAS_EQM_comm_repet_day1_HV_23_Dec_2019.jpg
Figure 5: HK profiles taken at EQM (MSSL) on 23 Dec 2019

1.2 5 Mar 2020, Rehearsal of Day 2 of commissioning

The main files are in Table 2
Table 2: Day Two commissioning files
I have performed actions as follows ( Time of EGSE is shifted against the time of MAC to 7 min back ):
  1. ON (05/03 15:40)
  2. Start Sequencer 15:41, OK
  3. Security configuration: 0x1A, 15:47, ОК
  4. MHV UP, 250V step, 16:03, OK
  5. Security configuration: 0x1F, then 0x07, 16:05, OK
  6. ON CEMs , 16:13, OK
  7. Start Static , N = 5000, , 16:13, OK
  8. CEM to 1000V step 200 V, 60s, 16:31, OK
  9. CEM HV nominal = 1850 V, OK
  10. Burst mode, 90,4,9,0, 44,3, K =4, N = 19, start 16:52, stop 17:00
  11. Standard Normal mode (N = 1) start 17:01 (05/03)
  12. The vacuum chamber accident at 9:07 06/03 (see below the accident description)
  13. The instrument was OFF at 10:23 06/03
The HK profiles for the experiment (for whole two days) are shown in Figure 6. The total CEM count, CEMs HV, and the corresponding currents are shown in Figure 7. Figure 8 shows the steps 1 - 10 (and start of item 11) with the zoom of the passage from the static scheme to the burst mode. Figure 9 shows the count and the corresponding HKs during the accident. It seems that the PAS count and the beam monitor were counting the ion scattered from the main ion beam due to the collisions in the vacuum chamber because of the low vacuum.
image: 5_home_fedorov_SOLARORB_PAS_FLIGHT_COMMISSIONING_DOCLOG_PAS_FS_comm_day_2_HV_09_Mar_2020.jpg
Figure 6: Left: HV for the whole time interval, Right: HV zoom for the accident time interval. Vertical red lines correspond to start of the accident and to the minimal vacuum (see Figure 9)
image: 6_home_fedorov_SOLARORB_PAS_FLIGHT_COMMISSIONING_DOCLOG_PAS_FS_comm_day_2_TotCount_09_Mar_2020.jpg
Figure 7: Total count, CEMs HV, and important currents for the whole time interval of the day 2.
image: 7_home_fedorov_SOLARORB_PAS_FLIGHT_COMMISSIONIN____comm_day_2_TotCount_Birst_Zoom_09_Mar_2020.jpg
Figure 8: Low panel: The interval at the beginning of the 2nd day of up the CEM voltage and Burst Mode. Upper panel: the zoom of the passage from the static mode to the burst mode.
image: 8_home_fedorov_SOLARORB_PAS_FLIGHT_COMMISSIONIN___PAS_FS_comm_day_2_TotCount_Zoom_09_Mar_2020.jpg
Figure 9: Low panel: the count, CEM HV and the current during the accident, Upper panel: the vacuum profile and the beam monitor current