All,
The perigee contacts were nominal. The inertial maneuver was successful. The SSR was dumped with 0 errors AND THE HI Gain Curve ATS was uplinked.
Tasks Accomplished:
Reset FDC Totals
SSR Dump -> Dump New
Reset Master Timer
CAR#1372 Hi Gain Curve ATS upload
IBEX_2024_063_o0640a_v001_HGC 64 Commands
Results from the Inertial Maneuver:
Q1 -0.60464400 ActNor.EstInrToBdy[0]
Q2 0.43695300 ActNor.EstInrToBdy[1]
Q3 -0.62173400 ActNor.EstInrToBdy[2]
Q4 0.23858600 ActNor.EstInrToBdy[3]
GPS sec 1393481309 ActNor.EstTime
UTC time
03/03/2024 06:08:15 output
MPS Diff
0.441 deg
MPS Cmd Vector X 0.95997300
MPS Cmd Vector Y -0.252847000
MPS Cmd Vector Z -0.120501000
CSS Angle TLM 1.36702
CSS Sun-Pointing Angle 2.73404
27 Feb 24 @15:00:00
CSS Angle TLM 0.86818
CSS Sun-Pointing Angle 1.73636
03 Mar 24 @06:00:00
Pre-Burn
Thruster 1 20144 27 Feb 24 @15:00:00
Thruster 2 19536
Thruster 3 27488
Thruster 4 28096
Post-Burn
Thruster 1 20512 03 Mar 24 @06:00:00
Thruster 2 19856
Thruster 3 27856
Thruster 4 28512
Number of Pulses
Thruster 1 368
Thruster 2 320
Thruster 3 368
Thruster 4 416
Thruster Pairs
Thruster 1 & 2 688
Thruster 3 & 4 784
Timothy E.Perry
CRS IBEX OCO-2
Mission Operations
Office (703) 406-5976
IBEX MOC (703)404-7470
Cell (301) 606-1430