All,

 

The perigee contacts were nominal for CMD and TLM. The Inertial maneuver was successful and battery balancing was nominal.

The following was completed:

               Reset Master Timer

               CAR #1017 ATS Upload – IBEX_2019_023_o0435a_v001.scr

               SSR Dump

               CAR #1016 – Re-dump orbit 432 problem blocks

 

Results from the Inertial Maneuver:

Q1 0.53833000  ActNor.EstInrToBdy[0]

Q2 -0.62564200 ActNor.EstInrToBdy[1]

Q3 0.54679700  ActNor.EstInrToBdy[2]

Q4 0.14066500  ActNor.EstInrToBdy[3]   

GPS sec 1231506695.000 ActNor.EstTime

MPS Cmd Vector X           0.417363000     

MPS Cmd Vector Y           -0.829655000    

MPS Cmd Vector Z            -0.370784000

MPS Diff 0.646 deg

CSS Angle TLM   1.60803

CSS Sun-Pointing Angle   3.21606

                              09 Jan 19 @19:00

CSS Angle TLM   0.754333            

CSS Sun-Pointing Angle   1.508666            

                              14 Jan 19 @13:00

Pre-Burn                          

Thruster 1            3888      09 Jan 19 @19:00

Thruster 2            3792     

Thruster 3            4672     

Thruster 4            4768     

Post-Burn                         

Thruster 1            4288      14 Jan 19 @13:00

Thruster 2            4192     

Thruster 3            5088     

Thruster 4            5184     

Number of Pulses                          

Thruster 1            400       

Thruster 2            400       

Thruster 3            416       

Thruster 4            416       

Thruster Pairs                  

Thruster 1 & 2    800       

Thruster 3 & 4    832       

 

 

Eric Chubin
Mission Operations Engineer - OCO2, IBEX
Northrop Grumman Innovation Systems

OCO2 MOC#: (703) 429 - 7015

Mobile#: (240) 328 - 2098

Eric.Chubin@ngc.com

 
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