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@ngc.com
Office (703) 406-5976
Cell (301) 606-1430

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