[Isocops] Goat Herder for 5 Feb 2019

[Perry, Timothy]

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 at ngc.com<mailto:timothy.perry at ngc.com>
Office (703) 406-5976
Cell (301) 606-1430

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