[Isocops] Goat Herder for Dec 13, 2018

[Perry, Timothy]

All,
The Apogee support was nominal for CMD and TLM. The Inertial maneuver was successful.

The results for the maneuver:
Q1 0.62413900 ActNor.EstInrToBdy[0]
Q2 -0.55425800 ActNor.EstInrToBdy[1]
Q3 0.29833200 ActNor.EstInrToBdy[2]
Q4 0.46286700 ActNor.EstInrToBdy[3]
GPS sec 1228770085.000 ActNor.EstTime
MPS Cmd Vector X -0.135262000
MPS Cmd Vector Y -0.905276000
MPS Cmd Vector Z -0.402715000
MPS Diff 0.640 deg
CSS Angle TLM 0.395153
CSS Sun-Pointing Angle 0.790306
  8 Dec 18 @16:30
CSS Angle TLM 0.785481
CSS Sun-Pointing Angle 1.570962
  13 Dec 18 @21:00
Pre-Burn
Thruster 1 2224 8 Dec 18 @16:30
Thruster 2 2176
Thruster 3 2368
Thruster 4 2416
Post-Burn
Thruster 1 2496 13 Dec 18 @21:00
Thruster 2 2448
Thruster 3 2672
Thruster 4 2720
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 at ngc.com<mailto:timothy.perry at ngc.com>
Office (703) 406-5976
Cell (301) 606-1430

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