All,
The Perigee passes were nominal for CMD and TLM. The Inertial maneuver was successful.
The following was accomplished:
Reset the Master Timer
SSR Dump -> Dump New
CAR #1070 ATS upload – IBEX_2019_314_o0467a_v001 81 Cmds
Results from the Inertial maneuver:
Q1 0.75908400
Q2 -0.19473400
Q3 -0.41845700
Q4 0.45909100
GPS sec 1256598137
MPS Diff
0.722 deg
MPS Cmd Vector X -0.811712000
MPS Cmd Vector Y -0.532222000
MPS Cmd Vector Z -0.240550000
CSS Angle TLM 0.296075
CSS Sun-Pointing Angle 0.59215
27 Oct 19 @ 23:00
CSS Angle TLM 1.00112
CSS Sun-Pointing Angle 2.00224
31 Oct 19 @ 22:15
Pre-Burn
Thruster 1 19664 27 Oct 19 @ 23:00
Thruster 2 19072
Thruster 3 25328
Thruster 4 25920
Post-Burn
Thruster 1 19904 31 Oct 19 @ 22:15
Thruster 2 19312
Thruster 3 25632
Thruster 4 26224
Number of Pulses
Thruster 1 240
Thruster 2 240
Thruster 3 304
Thruster 4 304
Thruster Pairs
Thruster 1 & 2 480
Thruster 3 & 4 608
Timothy E. Perry
Mission Operations
CRS, IBEX, OCO-2 & TESS
Office (703) 406-5976
Cell (301) 606-1430
