All,
The perigee passes were nominal for CMD and TLM. The Inertial maneuver was successful. As part of the string-2 recertification, I took the second pass on in it. CMD and TLM
was nominal.
The following was completed:
Reset the Master Timer
Set the Spacecraft Clock
Reset FDC totals
SSR Dump -> Dump_New
Results from the Inertial maneuver:
Q1 -0.57817200 ActNor.EstInrToBdy[0]
Q2 -0.22672800 ActNor.EstInrToBdy[1]
Q3 0.46072400 ActNor.EstInrToBdy[2]
Q4 0.63407000 ActNor.EstInrToBdy[3]
GPS sec 1250422185 ActNor.EstTime
MPS Diff 0.615 deg
MPS Cmd Vector X -0.822081000
MPS Cmd Vector Y 0.525925000
MPS Cmd Vector Z 0.218143000
CSS Angle TLM 0.815654
CSS Sun-Pointing Angle 1.631308
16 Aug 19 @ 12:00
CSS Angle TLM 0.467719
CSS Sun-Pointing Angle 0.935438
21 Aug 19 @ 11:30
Pre-Burn
Thruster 1 16512 16 Aug 19 @ 12:00
Thruster 2 16096
Thruster 3 19520
Thruster 4 19936
Post-Burn
Thruster 1 16752 21 Aug 19 @ 11:30
Thruster 2 16336
Thruster 3 19808
Thruster 4 20224
Number of Pulses
Thruster 1 240
Thruster 2 240
Thruster 3 288
Thruster 4 288
Thruster Pairs
Thruster 1 & 2 480
Thruster 3 & 4 576
Timothy E.Perry
CRS IBEX OCO-2
Mission Operations
tim.perry@ngc.com
Office (703) 406-5976
Cell (301) 606-1430