All, 

   The perigee contacts were nominal and the inertial maneuver was successful. We were able to set the spacecraft clock. We reset the master timer and reset FDC totals. The ATS for orbit #576 was uplinked. 

 

 

 

Tasks Accomplished: 

Reset FDC Totals 

SSR Dump -> Dump New 

Set Spacecraft Time 

Reset Master Timer 

CAR #1245 Orbit #576 ATS uplink 

   IBEX_2022_209_o0576a_v002 100 Cmds 

 

Results from the Inertial Maneuver: 

Q1 0.07040360 ActNor.EstInrToBdy[0] 

Q2 -0.55846200 ActNor.EstInrToBdy[1] 

Q3 -0.78356300 ActNor.EstInrToBdy[2] 

Q4 0.26303600 ActNor.EstInrToBdy[3] 

      

GPS sec 1342295384 ActNor.EstTime      

UTC time 07/19/2022 19:49:30 output 

 

MPS Diff 0.810 deg 

 

MPS Cmd Vector X -0.411305000 

MPS Cmd Vector Y 0.839839000 

MPS Cmd Vector Z 0.354258000 

 

CSS Angle TLM 0.326259  

CSS Sun-Pointing Angle 0.652518  

  15 July 22 @10:00:00 

 

CSS Angle TLM 0.27052  

CSS Sun-Pointing Angle 0.54104  

  19 July 22 @19:30:00 

 

Pre-Burn    

Thruster 1 2224 15 July 22 @10:00:00 

Thruster 2 2160  

Thruster 3 2704  

Thruster 4 2768  

 

Post-Burn    

Thruster 1 2512 19 July 22 @19:30:00 

Thruster 2 2448  

Thruster 3 2992  

Thruster 4 3056  

 

Number of Pulses    

Thruster 1 288  

Thruster 2 288  

Thruster 3 288  

Thruster 4 288  

Thruster Pairs   

Thruster 1 & 2 576  

Thruster 3 & 4 576