All,
The Apogee contact was nominal for CMD and TLM. The Inertial maneuver was successful. The commands for the upcoming APL-8 contact were removed and Orbit 499 Bus ATS was uplinked.
Tasks Accomplished:
CAR #1109 ATS upload – IBEX_2020_241_o0499a_BUS_V001 46
Cmds
All Timed commands for the APL-18 contact on 8/18 @14:00 have been removed from the spacecraft.
Results from the Inertial maneuver:
Q1 -0.25179200
ActNor.EstInrToBdy[0]
Q2 -0.55462800
ActNor.EstInrToBdy[1]
Q3 -0.19177900
ActNor.EstInrToBdy[2]
Q4 0.76955100
ActNor.EstInrToBdy[3
]
GPS sec 1281434544
ActNor.EstTime
UTC time 08/14/2020 10:02:10 output
MPS Diff 0.475
deg
MPS
Cmd Vector X -0.758530000
MPS
Cmd Vector Y 0.601785000
MPS
Cmd Vector Z 0.249974000
CSS Angle TLM 0.239031
CSS Sun-Pointing Angle 0.478062
9 Aug 20 @ 17:00
CSS Angle TLM 0.716525
CSS Sun-Pointing Angle 1.43305
14 Aug 20 @ 10:00
Pre-Burn
Thruster 1 2000 9 Aug 20 @ 17:00
Thruster 2 1936
Thruster 3 2304
Thruster 4 2368
Post-Burn
`
Thruster 1 2256 14 Aug 20 @ 10:00
Thruster 2 2192
Thruster 3 2608
Thruster 4 2672
Number of Pulses
Thruster 1 256
Thruster 2 256
Thruster 3 304
Thruster 4 304
Thruster Pairs
Thruster 1 & 2 512
Thruster 3 & 4 608
Timothy E. Perry
Mission Operations
CRS, IBEX, OCO-2
Office (703) 406-5976
Cell (301) 606-1430
