All,
The perigee contacts were nominal. The inertial maneuver was successful. The Orbit 463 ats was uplinked. The Hi background sweep table was successfully uplinked.
Tasks Accomplished:
SSR Dump -> Dump New
CAR # 1335 2024 ISN Season and Hi Background test sweep table uploads
Pass # 5 Upload Hi Background Sweep table
CAR # 1382 Orbit # 643 ATS upload
IBEX_2024)090_o0643a_v001 101 commands
Reset FDC Totals
Reset Master Timer
Results from the Inertial Maneuver:
Q1 0.47996900 ActNor.EstInrToBdy[0]
Q2 0.51852200 ActNor.EstInrToBdy[1]
Q3 0.47968800 ActNor.EstInrToBdy[2]
Q4 0.52025400 ActNor.EstInrToBdy[3]
GPS sec 1395076040 ActNor.EstTime
UTC time
03/21/2024 17:07:06 output
MPS Diff
0.818 deg
MPS Cmd Vector X 0.99993000
MPS Cmd Vector Y 0.010454000
MPS Cmd Vector Z -0.005515000
CSS Angle TLM 0.974179
CSS Sun-Pointing Angle 1.948358
16 Mar 24 @13:00:00
CSS Angle TLM 0.773796
CSS Sun-Pointing Angle 1.547592
21 Mar 24 @17:00:00
Pre-Burn
Thruster 1 21344 16 Mar 24 @13:00:00
Thruster 2 20688
Thruster 3 28752
Thruster 4 29408
Post-Burn
Thruster 1 21520 21 Mar 24 @17:00:00
Thruster 2 20864
Thruster 3 28944
Thruster 4 29600
Number of Pulses
Thruster 1 176
Thruster 2 176
Thruster 3 192
Thruster 4 192
Thruster Pairs
Thruster 1 & 2 352
Thruster 3 & 4 384
Timothy E.Perry
CRS IBEX OCO-2
Mission Operations
Office (703) 406-5976
IBEX MOC (703)404-7470
Cell (301) 606-1430