All,

   The pass’s were nominal for CMD and TLM. The inertial maneuver was successful.

Completed CAR #998 ATS uplink – IBEX_2018_280_o0423a_v001 88 cmds

Dumped the SSR and set pointers to 6500

Reset Master Timer

Cleared FDC total

 

Maneuver Results:

Q1 0.44588100 ActNor.EstInrToBdy[0]

Q2 -0.55637600 ActNor.EstInrToBdy[1]

Q3 -0.41657700 ActNor.EstInrToBdy[2]

Q4 0.56400400 ActNor.EstInrToBdy[3]

GPS sec 1222172911.000 ActNor.EstTime

MPS Cmd Vector X -0.998671000

MPS Cmd Vector Y -0.042869000

MPS Cmd Vector Z -0.028602000

MPS Diff 0.710

CSS Angle TLM 1.84737

CSS Sun-Pointing Angle 3.69474

  24 Sept 18 @ 09:00

CSS Angle TLM 0.333965

CSS Sun-Pointing Angle 0.66793

  28 Sept 18 @ 12:30

Pre-Burn   

Thruster 1 6112 24 Sept 18 @ 09:00

Thruster 2 5952

Thruster 3 6560

Thruster 4 6720

Post-Burn  

Thruster 1 6384 28 Sept 18 @ 12:30

Thruster 2 6224

Thruster 3 6848

Thruster 4 7008

Number of Pulses  

Thruster 1 272

Thruster 2 272

Thruster 3 288

Thruster 4 288

Thruster Pairs 

Thruster 1 & 2 544

Thruster 3 & 4 576

 

 

 

 

Timothy E. Perry

CRS, IBEX, OCO-2 & TESS

Mission Operations

Tim.perry@ngc.com

Office (703) 406-5976

Cell (301) 606-1430

 

 



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