All,
The perigee passes were nominal for CMD and TLM. The Inertial maneuver was successful.
The following was accomplished:
CAR#1009 IESN season and Hi background table uploads
Completed pass 1 - Uplinked the following tables – Table_Hi_023456_Background and Table_Lo_11223678_ISN2
CAR#1011 ATS upload – IBEX_2018_352_o0431a_v001 91 cmds
Reset the Master timer
SSR Dump
Results from the Inertial maneuver:
Q1 0.21526400 ActNor.EstInrToBdy[0]
Q2 0.80463000 ActNor.EstInrToBdy[1]
Q3 -0.55318500 ActNor.EstInrToBdy[2]
Q4 0.01477660 ActNor.EstInrToBdy[3]
GPS sec 1228321793.000
ActNor.EstTime
MPS Cmd Vector X -0.211893000
MPS Cmd Vector Y -0.892545000
MPS Cmd Vector Z -0.398077000
MPS Diff 0.661 deg
MPS Diff 0.661 deg
CSS Angle TLM 0.97438
CSS Sun-Pointing Angle 1.94876
7 Dec 18 @13:00
CSS Angle TLM 0.395153
CSS Sun-Pointing Angle 0.790306
8 Dec 18 @16:30
Pre-Burn
Thruster 1 1856 7 Dec 18 @13:00
Thruster 2 1808
Thruster 3 1952
Thruster 4 2000
Post-Burn
Thruster 1 2224 8 Dec 18 @16:30
Thruster 2 2176
Thruster 3 2368
Thruster 4 2416
Number of Pulses
Thruster 1 368
Thruster 2 368
Thruster 3 416
Thruster 4 416
Thruster Pairs
Thruster 1 & 2 736
Thruster 3 & 4 832
Timothy E. Perry
Mission Operations
CRS, IBEX, OCO-2 & TESS
RAPTOR Test Team
Office (703) 406-5976
Cell (301) 606-1430