All,

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

Results of the maneuver:

 

0.70736200 ActNor.EstInrToBdy[0]

-0.43421500 ActNor.EstInrToBdy[1]

0.10898200 ActNor.EstInrToBdy[2]

0.54700900 ActNor.EstInrToBdy[3]

1228222842.000 ActNor.EstTime

MPS Cmd Vector X -0.317803000

MPS Cmd Vector Y -0.865955000

MPS Cmd Vector Z -0.386164000

MPS Diff 0.532 deg

CSS Angle TLM 0.483355

CSS Sun-Pointing Angle 0.96671

  29  Nov 18 @19:30

CSS Angle TLM 0.97438

CSS Sun-Pointing Angle 1.94876

  7 Dec 18 @13:00

Pre-Burn   

Thruster 1 1392 29  Nov 18 @19:30

Thruster 2 1392

Thruster 3 1504

Thruster 4 1504

Post-Burn  

Thruster 1 1856 7 Dec 18 @13:00

Thruster 2 1808

Thruster 3 1952

Thruster 4 2000

Number of Pulses  

Thruster 1 464

Thruster 2 416

Thruster 3 448

Thruster 4 496

Thruster Pairs 

Thruster 1 & 2 880

Thruster 3 & 4 944

 

 

 

 

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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