All,
The pass was nominal for CMD and TLM. The Inertial maneuver was successful.
Results from the maneuver:
Q1 -0.23682800 ActNor.EstInrToBdy[0]
Q2 -0.52856800 ActNor.EstInrToBdy[1]
Q3 -0.40584400 ActNor.EstInrToBdy[2]
Q4 0.70697900 ActNor.EstInrToBdy[3]
MPS Cmd Vector X -0.556844000
MPS Cmd Vector Y 0.766065000
MPS Cmd Vector Z 0.321043000
GPS sec 1248523178 ActNor.EstTime
UTC time 07/30/2019 11:59:24 output
MPS Diff 0.487 deg
CSS Angle TLM 1.46714
CSS Sun-Pointing Angle 2.93428
25 July 19 @ 11:00
CSS Angle TLM 0.569239
CSS Sun-Pointing Angle 1.138478
30 July 19 @ 12:00
Pre-Burn
Thruster 1 15184 25 July 19 @ 11:00
Thruster 2 14800
Thruster 3 18064
Thruster 4 18448
Post-Burn
Thruster 1 15440 30 July 19 @ 12:00
Thruster 2 15056
Thruster 3 18368
Thruster 4 18752
Number of Pulses
Thruster 1 256
Thruster 2 256
Thruster 3 304
Thruster 4 304
Thruster Pairs
Thruster 1 & 2 512
Thruster 3 & 4 608
Timothy E.Perry
CRS IBEX OCO-2
Mission Operations
tim.perry@ngc.com
Office (703) 406-5976
Cell (301) 606-1430
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