All,

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

The following was completed during these contacts:

Reset Master Timer

Set Spacecraft Clock

Reset FDC totals

SSR Dump _Dump New

FC Back Orbit dump

CAR 1025 ATS upload – IBEX _2019_069_o0440a_v001 – 81 cmds

 

Results from the Inertial maneuver:

Q1 -0.45747400 ActNor.EstInrToBdy[0]

Q2 0.59648600 ActNor.EstInrToBdy[1]

Q3 -0.54108800 ActNor.EstInrToBdy[2]

Q4 0.37702200 ActNor.EstInrToBdy[3]

GPS sec 1235435495.000 ActNor.EstTime

MPS Diff 0.707 deg

MPS Cmd Vector X 0.946998000

MPS Cmd Vector Y -0.290539000

MPS Cmd Vector Z -0.137047000

CSS Angle TLM 0.600357

CSS Sun-Pointing Angle 1.200714

  26 Feb 19 @18:00

CSS Angle TLM 0.479698

CSS Sun-Pointing Angle 0.959396

  01 Mar 19 @00:30

Pre-Burn   

Thruster 1 6720 26 Feb 19 @18:00

Thruster 2 6576

Thruster 3 8112

Thruster 4 8256

Post-Burn  

Thruster 1 6976 01 Mar 19 @00:30

Thruster 2 6832

Thruster 3 8384

Thruster 4 8528

Number of Pulses  

Thruster 1 256

Thruster 2 256

Thruster 3 272

Thruster 4 272

Thruster Pairs 

Thruster 1 & 2 512

Thruster 3 & 4 544

 

 

 

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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