All,

    The perigee contacts were nominal for CMD and TLM. The Inertial maneuver was successful.

The following was completed:

CAR 1006 ATS Upload – IBEX_2018_325_o0428a_LGC_V001

Reset Master Timer

SSR Dump and reset the pointers to 6500

Set the SC Clock

Reset FDC Totals

 

Results from the Inertial maneuver:

Q1 0.79563000 ActNor.EstInrToBdy[0]

Q2 -0.17275700 ActNor.EstInrToBdy[1]

Q3 -0.24091300 ActNor.EstInrToBdy[2]

Q4 0.52828900 ActNor.EstInrToBdy[3]

GPS sec 1226772670.000 ActNor.EstTime

MPS Cmd Vector X -0.559607000

MPS Cmd Vector Y -0.756679000

MPS Cmd Vector Z -0.338048000

MPS Diff 0.794 deg

CSS Angle TLM 1.35595

CSS Sun-Pointing Angle 2.7119

  18  Nov 18 @ 04:30

CSS Angle TLM 1.35595

CSS Sun-Pointing Angle 2.7119

  20  Nov 18 @ 18:00

Pre-Burn   

Thruster 1 544 18  Nov 18 @ 04:30

Thruster 2 544

Thruster 3 592

Thruster 4 592

Post-Burn  

Thruster 1 816 20  Nov 18 @ 18:00

Thruster 2 816

Thruster 3 896

Thruster 4 896

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

RAPTOR Test Team

timothy.perry@ngc.com

Office (703) 406-5976

Cell (301) 606-1430

 

 
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