[Isocops] IBEX Goat Herder for 3 March2024

[Perry, Timothy E [US] (SP)]

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
timothy.perry at ngc.com<mailto:timothy.perry at ngc.com>
Office (703) 406-5976
IBEX MOC (703)404-7470
Cell (301) 606-1430

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