All,

 

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

The following was completed:

               CAR #1010 ATS Upload – IBEX_2018_343_o0430a_v001.scr

               SSR Dump

               Reset Master Timer

               Set the SC Clock

               Dump FC Back Orbit Data

 

Results from the Inertial Maneuver:

Q1 0.69344300 ActNor.EstInrToBdy[0]

Q2 0.44376900 ActNor.EstInrToBdy[1]

Q3 -0.49072400 ActNor.EstInrToBdy[2]

Q4 0.28530000 ActNor.EstInrToBdy[3]

GPS sec 1227555100.000 ActNor.EstTime

MPS Cmd Vector X -0.420876000

MPS Cmd Vector Y -0.828588000

MPS Cmd Vector Z -0.369195000

MPS Diff 0.877 deg

CSS Angle TLM   1.70949

CSS Sun-Pointing Angle   3.41898

               27  Nov 18 @23:30

CSS Angle TLM   0.483355            

CSS Sun-Pointing Angle   0.96671

               29  Nov 18 @19:30

Pre-Burn                          

Thruster 1 1120  27  Nov 18 @23:30

Thruster 2 1120 

Thruster 3 1200 

Thruster 4 1200 

Post-Burn                         

Thruster 1 1392  29  Nov 18 @19:30

Thruster 2 1392 

Thruster 3 1504 

Thruster 4 1504 

Number of Pulses                          

Thruster 1 272   

Thruster 2 272   

Thruster 3 304   

Thruster 4 304   

Thruster Pairs                  

Thruster 1 & 2    544       

Thruster 3 & 4    608       

 

 

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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