All, 

    The spacecraft is nominal and the inertial maneuver was successful.  The STA spin rate looks valid. The rate changed from 4.177 to 4.181 post maneuver.  

 

Results from the Inertial Maneuver: 

Q1 0.24886700 ActNor.EstInrToBdy[0] 

Q2 -0.56795000 ActNor.EstInrToBdy[1] 

Q3 -0.65702200 ActNor.EstInrToBdy[2] 

Q4 0.42874300 ActNor.EstInrToBdy[3] 

      

GPS sec 1345082508 ActNor.EstTime 

UTC time 08/21/2022 02:01:34 output 

 

MPS Diff 0.631 deg 

 

MPS Cmd Vector X -0.816774000 

MPS Cmd Vector Y 0.533241000 

MPS Cmd Vector Z 0.220306000 

 

CSS Angle TLM 0.775817  

CSS Sun-Pointing Angle 1.551634  

  15 Aug 22 @16:30:00 

 

CSS Angle TLM 0.527119  

CSS Sun-Pointing Angle 1.054238  

  21 Aug 22 @02:00:00 

 

Pre-Burn    

Thruster 1 4176 15 Aug 22 @16:30:00 

Thruster 2 4080  

Thruster 3 4720  

Thruster 4 4816  

Post-Burn    

Thruster 1 4448 21 Aug 22 @02:00:00 

Thruster 2 4352  

Thruster 3 5040  

Thruster 4 5136  

Number of Pulses    

Thruster 1 272  

Thruster 2 272  

Thruster 3 320  

Thruster 4 320  

Thruster Pairs   

Thruster 1 & 2 544  

Thruster 3 & 4 640