[Isocops] IBEX Goat Herder for Oct 27

[Chubin, Eric [US] (IS)]

All,



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



Results from the Inertial Maneuver:

CSS Angle TLM   0.863208
CSS Sun-Pointing Angle   1.726416
  22 Oct 19 @ 23:05
CSS Angle TLM   0.296075
CSS Sun-Pointing Angle   0.59215
  27 Oct 19 @ 23:00
Pre-Burn
Thruster 1 19520 22 Oct 19 @ 23:05
Thruster 2 18928
Thruster 3 25136
Thruster 4 25728
Post-Burn
Thruster 1 19664 27 Oct 19 @ 23:00
Thruster 2 19072
Thruster 3 25328
Thruster 4 25920
Number of Pulses
Thruster 1 144
Thruster 2 144
Thruster 3 192
Thruster 4 192
Thruster Pairs
Thruster 1 & 2    288
Thruster 3 & 4    384


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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