All,
The perigee contacts for Orbit 415 were nominal for CMD and TLM.
The following was completed:
CAR 987 ATS upload IBEX_2018_o0417a_v001 97 CMDS
Dumped SSR
CAR 988 Dump Orbit 415 missing blocks
Reset Master Timer
Reset FDC Totals
Set the SC Clock
The Inertial maneuver was successful.
Q1 -0.55739000 ActNor.EstInrToBdy[0]
Q2 -0.19097200 ActNor.EstInrToBdy[1]
Q3 0.32368800 ActNor.EstInrToBdy[2]
Q4 0.74031900 ActNor.EstInrToBdy[3]
GPS sec
1217508180.000 ActNor.EstTime
MPS Diff
0.638
MPS Cmd Vector X -0.646303000
MPS Cmd Vector Y 0.703736000
MPS Cmd Vector Z 0.295041000
CSS Angle TLM 0.310274
CSS Sun-Pointing Angle 0.620548
31 July 18 @1100
CSS Angle TLM 0.310274
CSS Sun-Pointing Angle 0.620548
05 Aug 18 @1200
Pre-Burn
Thruster 1 2720 31 July 18 @1100
Thruster 2 2656
Thruster 3 3040
Thruster 4 3104
Post-Burn
Thruster 1 2992 05 Aug 18 @1200
Thruster 2 2928
Thruster 3 3344
Thruster 4 3408
Number of Pulses
Thruster 1 272
Thruster 2 272
Thruster 3 304
Thruster 4 304
Thruster Pairs
Thruster 1 & 2 544
Thruster 3 & 4 608
Timothy E. Perry
CRS, IBEX, OCO-2 & TESS
Mission Operations
Office (703) 406-5976
Cell (301) 606-1430
Corp Cell (571) 447-8977