All,
The perigee contacts were nominal. The inertial maneuver was successful. We dumped the SSR data for orbit 630. We were able to redump missing data from both orbits 629 & 630. The orbit 632 ATS was uplinked.
Tasks Accomplished:
CAR #1359 Redump missing orbit 629 blocks
CAR #1360 Orbit 632 ATS upload
IBEX_2023_354_o0632a_v001 108 cmds
CAR #1361 Redump missing orbit 630 blocks
Set Spacecraft clock
Dumped Flight Computer Back Orbit Data
Reset FDC Totals
Reset Master Timer
Results from the Inertial Maneuver:
Q1 0.25915800 ActNor.EstInrToBdy[0]
Q2 -0.79274700 ActNor.EstInrToBdy[1]
Q3 0.47983600 ActNor.EstInrToBdy[2]
Q4 0.27229700 ActNor.EstInrToBdy[3]
GPS sec 1386302522 ActNor.EstTime
UTC time
12/11/2023 04:01:48 output
MPS Diff
0.652 deg
MPS Cmd Vector X -0.17728000
MPS Cmd Vector Y -0.898951000
MPS Cmd Vector Z -0.400573000
CSS Angle TLM 1.24678
CSS Sun-Pointing Angle 2.49356
06 Dec 23 @23:30:00
CSS Angle TLM 1.14261
CSS Sun-Pointing Angle 2.28522
11 Dec 23 @04:00:00
Pre-Burn
Thruster 1 15808 06 Dec 23 @23:30:00
Thruster 2 15344
Thruster 3 20960
Thruster 4 21424
Post-Burn
Thruster 1 16144 11 Dec 23 @04:00:00
Thruster 2 15680
Thruster 3 21296
Thruster 4 21760
Number of Pulses
Thruster 1 336
Thruster 2 336
Thruster 3 336
Thruster 4 336
Thruster Pairs
Thruster 1 & 2 672
Thruster 3 & 4 672
Timothy E.Perry
CRS IBEX OCO-2
Mission Operations
Office (703) 406-5976
Cell (301) 606-1430