All,
The Apogee contact was nominal for CMD and TLM. The Inertial maneuver was successful.
Tim
Results from the maneuver:
Q1 0.76024100
ActNor.EstInrToBdy[0]
Q2 -0.02112620
ActNor.EstInrToBdy[1]
Q3 0.60987300
ActNor.EstInrToBdy[2]
Q4 0.22280400
ActNor.EstInrToBdy[3]
GPS sec
1235239330.000 ActNor.EstTime
MPS Cmd Vector X 0.918417000
MPS Cmd Vector Y -0.359184000
MPS Cmd Vector Z -0.165822000
MPS Diff
0.601 deg
CSS Angle TLM 0.581482
CSS Sun-Pointing Angle 1.162964
20 Feb 19 @01:00
CSS Angle TLM 0.624637
CSS Sun-Pointing Angle 1.249274
26 Feb 19 @18:00
Pre-Burn
Thruster 1 6336 20 Feb 19 @01:00
Thruster 2 6192
Thruster 3 7664
Thruster 4 7808
Post-Burn
Thruster 1 6720 26 Feb 19 @18:00
Thruster 2 6576
Thruster 3 8112
Thruster 4 8256
Number of Pulses
Thruster 1 384
Thruster 2 384
Thruster 3 448
Thruster 4 448
Thruster Pairs
Thruster 1 & 2 768
Thruster 3 & 4 896
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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