[Isocops] IBEX Goat Herder for 02 Dec 2019

[Chubin, Eric [US] (IS)]

All,

The Apogee pass was nominal for CMD and TLM. The Inertial maneuver was successful.

Results from the Inertial maneuver:
Q1 0.67234300 ActNor.EstInrToBdy[0]
Q2 0.48289500 ActNor.EstInrToBdy[1]
Q3 -0.47271900 ActNor.EstInrToBdy[2]
Q4 0.30216500 ActNor.EstInrToBdy[3]
GPS sec 1259364781 ActNor.EstTime

UTC time 12/02/2019 23:32:47 output
MPS Diff 0.750 deg
CSS Angle TLM   0.561277
CSS Sun-Pointing Angle   1.122554
               28 Nov 19 @ 23:30
CSS Angle TLM   0.900921
CSS Sun-Pointing Angle   1.801842
               02 Dec 19 @ 23:30

Pre-Burn
Thruster 1 21264 28 Nov 19 @ 01:30
Thruster 2 20592
Thruster 3 27888
Thruster 4 28560
Post-Burn
Thruster 1 21680 02 Dec 19 @ 23:30
Thruster 2 21008
Thruster 3 28320
Thruster 4 28992
Number of Pulses
Thruster 1 416
Thruster 2 416
Thruster 3 432
Thruster 4 432
Thruster Pairs
Thruster 1 & 2    832
Thruster 3 & 4    864


Eric Chubin
Mission Operations Engineer - OCO2, IBEX
Northrop Grumman Innovation Systems
OCO2 MOC#: (703) 429 - 7015
Mobile#: (240) 328 - 2098
Eric.Chubin at ngc.com

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