All,

   The perigee contacts were successful for CMD and TLM. The second contact had uplink issues at the beginning of the contact. The reason for the issue is still under investigation. The Inertial maneuver was successful.

 

The following commanding was completed:

Reset Master Timer

SSR Dump -> Dump new and reset the pointers to 70000

CAR #1042 IBEX Hi Background test and Lo magneto tail Season

   Completed Pass #2 – Upload Hi Normal and Lo Magneto tail sweep tables.

CAR #1046 upload ATS Orbit #453

   IBEX_2019_188_o0453a_V001 93 Cmds

CAR #1044 upload ATS Orbit #452 APL contact

   IBEX_2019_o0452a_APL18_V001 6 Cmds

CAR #1045 upload ATS Orbit #453 APL contact

   IBEX_2019_o0453a_APL18_V001 7 Cmds

 

 

Results frm the maneuver:

Q1 -0.53781400 ActNor.EstInrToBdy[0]

Q2 0.11095200 ActNor.EstInrToBdy[1]

Q3 0.22708700 ActNor.EstInrToBdy[2]

Q4 0.80428600 ActNor.EstInrToBdy[3]

GPS sec 1245783798 ActNor.EstTime

MPS Diff 0.524 deg

MPS Cmd Vector X -0.066571000

MPS Cmd Vector Y 0.919042000

MPS Cmd Vector Z 0.388497000

CSS Angle TLM 0.737544

CSS Sun-Pointing Angle 1.475088

  24 June 19 @ 13:00

CSS Angle TLM 1.26594

CSS Sun-Pointing Angle 2.53188

  28 June 19 @ 03:00

Pre-Burn   

Thruster 1 13424 24 June 19 @ 13:00

Thruster 2 13104

Thruster 3 15920

Thruster 4 16240

Post-Burn  

Thruster 1 13696 28 June 19 @ 03:00

Thruster 2 13376

Thruster 3 16224

Thruster 4 16544

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

 

Timothy E. Perry

Mission Operations

CRS, IBEX, OCO-2 & TESS

timothy.perry@ngc.com

Office (703) 406-5976

Cell (301) 606-1430

 

 



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