All,

 

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

The following was completed:

               SSR Dump

               Reset Master Timer

               CAR #1024 ATS Upload – IBEX_2019_060_o0439a_v001.scr

 

Results from the Sun Maneuver:

CSS Angle TLM   0.870207            

CSS Sun-Pointing Angle   1.740414            

               16 Feb 19 @17:30

CSS Angle TLM   0.581482            

CSS Sun-Pointing Angle   1.162964

                              20 Feb 19 @01:00

Pre-Burn                          

Thruster 1 6272  16 Feb 19 @17:30

Thruster 2 6128 

Thruster 3 7344 

Thruster 4 7488 

Post-Burn                         

Thruster 1 6336  20 Feb 19 @01:00

Thruster 2 6192 

Thruster 3 7664 

Thruster 4 7808 

Number of Pulses                          

Thruster 1 64     

Thruster 2 64     

Thruster 3 320   

Thruster 4 320   

Thruster Pairs                  

Thruster 1 & 2 128           

Thruster 3 & 4 640           

 

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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