All,
The 2 SSC passes were nominal for CMD and TLM. The Inertial maneuver was successful.
The following was accomplished:
CAR #993 ATS upload
IBEX_2018_253_o0420a_v001
97 Cmds, Trk #’s 576 – 672
Reset Master Timer
Set SC Clock
Reset FDC totals
Dumped FC Back Orbit Data
We are still waiting on the SSR dump data from APL. They have been notified and will be checking on it’s status.
Results of the Inertial maneuverP
Q1 0.52471900 ActNor.EstInrToBdy[0]
Q2 -0.37854100 ActNor.EstInrToBdy[1]
Q3 -0.74043300 ActNor.EstInrToBdy[2]
Q4 0.18203400 ActNor.EstInrToBdy[3]
GPS sec
1219874478.000 ActNor.EstTime
MPS Diff
0.799
MPS Cmd Vector X -0.917956000
MPS Cmd Vector Y 0.367509000
MPS Cmd Vector Z 0.149311000
CSS Angle TLM 0.63919
CSS Sun-Pointing Angle 1.27838
28 Aug 18 @1100
CSS Angle TLM 0.582827
CSS Sun-Pointing Angle 1.165654
01 Sept 18 @2200
Pre-Burn
Thruster 1 4416 28 Aug 18 @1100
Thruster 2 4288
Thruster 3 4800
Thruster 4 4928
Post-Burn
Thruster 1 4704 01 Sept 18 @2200
Thruster 2 4576
Thruster 3 5088
Thruster 4 5218
Number of Pulses
Thruster 1 288
Thruster 2 288
Thruster 3 288
Thruster 4 290
Thruster Pairs
Thruster 1 & 2 576
Thruster 3 & 4 578
Timothy E. Perry
CRS, IBEX, OCO-2 & TESS
Mission Operations
Office (703) 406-5976
Cell (301) 606-1430