All,
The apogee contact was nominal. The inertial maneuver was successful. We were able to switch over to maestro string3 and checkout the system. Initial checks
look good.
Results from the inertial Maneuver:
Q1 -0.65458300 ActNor.EstInrToBdy[0]
Q2 -0.02618350 ActNor.EstInrToBdy[1]
Q3 0.70427900 ActNor.EstInrToBdy[2]
Q4 0.27354500 ActNor.EstInrToBdy[3]
GPS sec 1409527910 ActNor.EstTime
UTC time
09/04/2024 23:31:36 output
MPS Diff
0.772 deg
MPS Cmd Vector X -0.93846700
MPS Cmd Vector Y 0.32061400
MPS Cmd Vector Z 0.12839800
CSS Angle TLM 0.338041
CSS Sun-Pointing Angle 0.676082
30 Aug 24 @21:00:00
CSS Angle TLM 0.449805
CSS Sun-Pointing Angle 0.89961
04 Sept 24 @23:30:00
Pre-Burn
Thruster 1 4944 30 Aug 24 @21:00:00
Thruster 2 4848
Thruster 3 5184
Thruster 4 5280
Post-Burn
Thruster 1 5216 04 Sept 24 @23:30:00
Thruster 2 5120
Thruster 3 5472
Thruster 4 5568
Number of Pulses
Thruster 1 272
Thruster 2 272
Thruster 3 288
Thruster 4 288
Thruster Pairs
Thruster 1 & 2 544
Thruster 3 & 4 576
Timothy E.Perry
CRS IBEX OCO-2
Mission Operations
Office (703) 406-5976
IBEX MOC (703)404-7470
Cell (301) 606-1430