All,
The Perigee passes were nominal for CMD and TLM. The Inertial maneuver was successful. The star tracker had reset earlier in the orbit. Time of the reset was Dec 9 (343) @03:24:13gmt.
Tasks accomplished:
Reset Master Timer
Set SC clock
SSR Dump -> Dump New
CAR #1078 Dump Missing blocks
CAR #1077 Orbit #472 ATS upload IBEX_2019_360_o0472a_v001 86
Cmds
CAR #1063 ISN and Hi background sweep tables. Completed Pass#3 Table_Hi_023456_Background
Star Tracker Image Dump – Uncompressed
Results from the Inertial maneuver:
Q1 0.43366800
ActNor.EstInrToBdy[0]
Q2 -0.71496300
ActNor.EstInrToBdy[1]
Q3 0.44537800
ActNor.EstInrToBdy[2]
Q4 0.31999900
ActNor.EstInrToBdy[3]
GPS sec 1260619320
ActNor.EstTime
UTC time
12/17/2019 12:01:46 output
MPS Diff
0.486 deg
MPS
Cmd Vector X -0.069298000
MPS
Cmd Vector Y -0.911205000
MPS
Cmd Vector Z -0.406083000
CSS Angle TLM 0.289391
CSS Sun-Pointing Angle 0.578782
16 Dec 19 @ 01:30
CSS Angle TLM 1.69084
CSS Sun-Pointing Angle 3.38168
17 Dec 19 @ 12:00
Pre-Burn
Thruster 1 704 16 Dec 19 @ 01:30
Thruster 2 704
Thruster 3 752
Thruster 4 752
Post-Burn
Thruster 1 992 17 Dec 19 @ 12:00
Thruster 2 992
Thruster 3 1088
Thruster 4 1088
Number of Pulses
Thruster 1 288
Thruster 2 288
Thruster 3 336
Thruster 4 336
Thruster Pairs
Thruster 1 & 2 576
Thruster 3 & 4 672
Timothy E. Perry
Mission Operations
CRS, IBEX, OCO-2 & TESS
Office (703) 406-5976
Cell (301) 606-1430
