All,
The Perigee contacts were nominal for CMD and TLM. The Inertial maneuver was successful.
The following was completed during these contacts:
CAR #978 IBEX-Hi Background test and Lo Magneto tail season
Completed Pass #3 Upload Background sweep table
Completed CAR #ATS upload – IBEX_2018_262_o0421a_V002 93 cmds
Dumped SSR
Reset the Master Timer
Set SC clock
Dumped FC Back orbit data
Reset FDC Totals
Results for the Inertial maneuver:
Q1 -0.14761600 ActNor.EstInrToBdy[0]
Q2 -0.65370700 ActNor.EstInrToBdy[1]
Q3 -0.01154990 ActNor.EstInrToBdy[2]
Q4 0.74212100 ActNor.EstInrToBdy[3]
GPS sec
1220630656.000 ActNor.EstTime
MPS Diff
0.625
MPS Cmd Vector X -0.968216000
MPS Cmd Vector Y 0.232967000
MPS Cmd Vector Z 0.091015000
CSS Angle TLM 0.666466
CSS Sun-Pointing Angle 1.332932
06 Sept 18 @1000
CSS Angle TLM 0.773037
CSS Sun-Pointing Angle 1.546074
10 Sept 18 @1600
Pre-Burn
Thruster 1 4976 06 Sept 18 @1000
Thruster 2 4848
Thruster 3 5376
Thruster 4 5504
Post-Burn
Thruster 1 5264 10 Sept 18 @1600
Thruster 2 5136
Thruster 3 5680
Thruster 4 5808
Number of Pulses
Thruster 1 288
Thruster 2 288
Thruster 3 304
Thruster 4 304
Thruster Pairs
Thruster 1 & 2 576
Thruster 3 & 4 608
Timothy E. Perry
CRS, IBEX, OCO-2 & TESS
Mission Operations
Office (703) 406-5976
Cell (301) 606-1430