All,

   The perigee contacts for Orbit 415 were nominal for CMD and TLM.

The following was completed:

CAR 987 ATS upload IBEX_2018_o0417a_v001 97 CMDS

Dumped SSR

CAR 988 Dump Orbit 415 missing blocks

Reset Master Timer

Reset FDC Totals

Set the SC Clock

 

The Inertial maneuver was successful.

 

Q1 -0.55739000 ActNor.EstInrToBdy[0]

Q2 -0.19097200 ActNor.EstInrToBdy[1]

Q3 0.32368800 ActNor.EstInrToBdy[2]

Q4 0.74031900 ActNor.EstInrToBdy[3]

GPS sec 1217508180.000 ActNor.EstTime

MPS Diff 0.638

MPS Cmd Vector X -0.646303000

MPS Cmd Vector Y 0.703736000

MPS Cmd Vector Z 0.295041000

CSS Angle TLM 0.310274

CSS Sun-Pointing Angle 0.620548

  31 July 18 @1100

CSS Angle TLM 0.310274

CSS Sun-Pointing Angle 0.620548

  05 Aug 18 @1200

Pre-Burn   

Thruster 1 2720 31 July 18 @1100

Thruster 2 2656

Thruster 3 3040

Thruster 4 3104

Post-Burn  

Thruster 1 2992 05 Aug 18 @1200

Thruster 2 2928

Thruster 3 3344

Thruster 4 3408

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

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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