[Isocops] Goat Herder for April 11

[Chubin, Eric]

All,

The apogee contact was nominal for CMD and TLM. The Inertial Maneuver was successful.

Results from the Inertial Maneuver:
Q1 -0.31261800 ActNor.EstInrToBdy[0]
Q2 0.58067800  ActNor.EstInrToBdy[1]
Q3 -0.14056000 ActNor.EstInrToBdy[2]
Q4 0.73846200  ActNor.EstInrToBdy[3]
GPS sec 1239026552.000 ActNor.EstTime
MPS Diff 0.626 deg
MPS Cmd Vector X           0.945101000
MPS Cmd Vector Y           0.303730000
MPS Cmd Vector Z            0.120553000
CSS Angle TLM   1.53468
CSS Sun-Pointing Angle   3.06936
                              6 Apr 19 @22:30
CSS Angle TLM   0.437455
CSS Sun-Pointing Angle   0.87491
                              11 Apr 19 @ 14:00
Pre-Burn
Thruster 1            8832      6 Apr 19 @22:30
Thruster 2            8608
Thruster 3            10880
Thruster 4            11104
Post-Burn
Thruster 1            9088      11 Apr 19 @ 14:00
Thruster 2            8864
Thruster 3            11184
Thruster 4            11408
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



Eric Chubin
Mission Operations Engineer - OCO2, IBEX
Northrop Grumman Innovation Systems
OCO2 MOC#: (703) 429 - 7015
Mobile#: (240) 328 - 2098
Eric.Chubin at ngc.com



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