All,

    The Apogee support was nominal for CMD and TLM. The Inertial maneuver was successful.

The ATS for Orbit #418 IBEX_2018_235_o0418a_v002 was uplinked.

Below are the results of the Inertial maneuver.

Q1 -0.60633400 ActNor.EstInrToBdy[0]

Q2 -0.11486700 ActNor.EstInrToBdy[1]

Q3 0.55616100 ActNor.EstInrToBdy[2]

Q4 0.55664200 ActNor.EstInrToBdy[3]

GPS sec 1218713629.000 ActNor.EstTime

UTC time 08/19/2018 11:33:35 output

MPS Diff 0.672

MPS Cmd Vector X -0.804154000

MPS Cmd Vector Y 0.549380000

MPS Cmd Vector Z 0.226974000

CSS Angle TLM 1.41817

CSS Sun-Pointing Angle 2.83634

  14 Aug 18 @1900

CSS Angle TLM 0.582827

CSS Sun-Pointing Angle 1.165654

  19 Aug 18 @1130

Pre-Burn   

Thruster 1 3600 14 Aug 18 @1900

Thruster 2 3472

Thruster 3 3952

Thruster 4 4080

Post-Burn  

Thruster 1 3872 19 Aug 18 @1130

Thruster 2 3744

Thruster 3 4240

Thruster 4 4368

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

Corp Cell (571) 447-8977

 

 



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