All,
The apogee contact was nominal for CMD and TLM. The inertial maneuver was successful.
Results from the Inertial maneuver:
Q1
0.61936300 ActNor.EstInrToBdy[0]
Q2 -0.25912900
ActNor.EstInrToBdy[1]
Q3 -0.73023900
ActNor.EstInrToBdy[2]
Q4 0.12645800
ActNor.EstInrToBdy[3]
GPS sec 1283825098
ActNor.EstTime
UTC time
09/11/2020 02:04:44 output
MPS Diff
0.749 deg
MPS
Cmd Vector X -0.971191000
MPS
Cmd Vector Y 0.222433000
MPS
Cmd Vector Z 0.085504000
CSS Angle TLM 0.304546
CSS Sun-Pointing Angle 0.609092
06 Sept 20 @ 20:00:00
CSS Angle TLM 0.517377
CSS Sun-Pointing Angle 1.034754
11 Sept 20 @ 02:00:00
Pre-Burn
Thruster 1 3600 06 Sept 20 @ 20:00:00
Thruster 2 3504
Thruster 3 4192
Thruster 4 4288
Post-Burn
`
Thruster 1 3872 11 Sept 20 @ 02:00:00
Thruster 2 3776
Thruster 3 4464
Thruster 4 4560
Number of Pulses
Thruster 1 272
Thruster 2 272
Thruster 3 272
Thruster 4 272
Thruster Pairs
Thruster 1 & 2 544
Thruster 3 & 4 544
Timothy E. Perry
Mission Operations
CRS, IBEX, OCO-2
Office (703) 406-5976
Cell (301) 606-1430
