All,
The perigee contacts were nominal for CMD and TLM. The Inertial Maneuver was successful.
The following was completed:
CAR #1092 ATS uplink – IBEX_2020_105_o0484a_HGA_V001 - 64
Cmds
CAR #1093 ATS uplink – IBEX_2020_113_o0485a_BUS_V001 – 40
Cmds
Set Spacecraft Time
Reset Master Timer
SSR Dump -> Dump New
Reset FDC Totals
Results from the Inertial Maneuver:
Q1 -0.62654800
Q2 -0.18388400
Q3 -0.75597400
Q4 0.04611920
MPS
Cmd Vector X 0.926693000
MPS
Cmd Vector Y 0.348302000
MPS
Cmd Vector Z 0.141160000
GPS sec 1270865238
UTC time 04/14/2020 02:07:04
MPS Diff 0.822
deg
CSS Angle TLM 0.0625
CSS Sun-Pointing Angle 0.125
9 Apr 20 @ 13:00
CSS Angle TLM 0.303902
CSS Sun-Pointing Angle 0.607804
14 Apr 20 @ 02:00
Pre-Burn
Thruster 1 7120 9 Apr 20 @ 13:00
Thruster 2 6928
Thruster 3 9376
Thruster 4 9568
Post-Burn
Thruster 1 7392 14 Apr 20 @ 02:00
Thruster 2 7168
Thruster 3 9648
Thruster 4 9872
Number of Pulses
Thruster 1 272
Thruster 2 240
Thruster 3 272
Thruster 4 304
Thruster Pairs
Thruster 1 & 2 512
Thruster 3 & 4 576
Timothy E. Perry
Mission Operations
CRS, IBEX, OCO-2 & TESS
Office (703) 406-5976
Cell (301) 606-1430
