All,

    The Apogee pass was nominal for CMD and TLM. The Inertial maneuver was nominal.

     

Results from the Inertial maneuver:

 

Q1 -0.12866000 ActNor.EstInrToBdy[0]

Q2 0.78531200 ActNor.EstInrToBdy[1]

Q3 -0.45694500 ActNor.EstInrToBdy[2]

Q4 0.39740700 ActNor.EstInrToBdy[3]

GPS sec 1233432126.000 ActNor.EstTime

MPS Cmd Vector X 0.742565000

MPS Cmd Vector Y -0.610753000

MPS Cmd Vector Z -0.274916000

MPS Diff 0.549 deg

CSS Angle TLM 0.30066

CSS Sun-Pointing Angle 0.60132

  1 Feb 19 @06:00

CSS Angle TLM 0.43924

CSS Sun-Pointing Angle 0.87848

  5 Feb 19 @20:00

Pre-Burn   

Thruster 1 5408 1 Feb 19 @06:00

Thruster 2 5264

Thruster 3 6416

Thruster 4 6560

Post-Burn  

Thruster 1 5696 5 Feb 19 @20:00

Thruster 2 5552

Thruster 3 6720

Thruster 4 6864

Number of Pulses  

Thruster 1 288

Thruster 2 288

Thruster 3 304

Thruster 4 304

Thruster Pairs  

Thruster 1 & 2 576

Thruster 3 & 4 608

 

 

 

Timothy E. Perry

Mission Operations

CRS, IBEX, OCO-2 & TESS

RAPTOR Test Team

timothy.perry@ngc.com

Office (703) 406-5976

Cell (301) 606-1430

 

 



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