All,
The perigee contacts were nominal for CMD and TLM. The Inertial maneuver was successful and battery balancing was nominal.
The following was completed:
SSR Dump
Reset Master Timer
CAR #1015 ATS Upload – IBEX_2019_014_o0434a_v001.scr
Reset FDC Totals
Results from the Inertial Maneuver:
Q1 0.78278100 ActNor.EstInrToBdy[0]
Q2 0.27884100 ActNor.EstInrToBdy[1]
Q3 -0.03303950 ActNor.EstInrToBdy[2]
Q4 0.55534700 ActNor.EstInrToBdy[3]
GPS sec 1230724725.000 ActNor.EstTime
MPS Cmd Vector X 0.265226000
MPS Cmd Vector Y -0.880525000
MPS Cmd Vector Z -0.392851000
MPS Diff 0.898 deg
CSS Angle TLM 1.13522
CSS Sun-Pointing Angle 2.27044
01 Jan 18 @20:00
CSS Angle TLM 0.85638
CSS Sun-Pointing Angle 1.71276
05 Jan 18 @12:00
Pre-Burn
Thruster 1 3408 01 Jan 18 @20:00
Thruster 2 3312
Thruster 3 3984
Thruster 4 4080
Post-Burn
Thruster 1 3776 05 Jan 18 @12:00
Thruster 2 3680
Thruster 3 4384
Thruster 4 4480
Number of Pulses
Thruster 1 368
Thruster 2 368
Thruster 3 400
Thruster 4 400
Thruster Pairs
Thruster 1 & 2 736
Thruster 3 & 4 800
Eric Chubin
Mission Operations Engineer - OCO2, IBEX
Northrop Grumman Innovation Systems
OCO2 MOC#: (703) 429 - 7015
Mobile#: (240) 328 - 2098
Eric.Chubin@ngc.com