All,
The Perigee passes were nominal for CMD and TLM. The Inertial maneuver was successful. The 18 day master timer command was sent as a timed command for future planning reference. The command was successful.
The following was completed:
Reset Master Timer
Reset FDC Totals
CAR # 1091 ATS upload IBEX_2020_105_o0484a_v001 96 CMDs
SSR Dump -> Dump New
Set Spacecraft time
EMR_StrobeMReset
$Time=2020/04:05:15:08:00
Results from the Inertial Maneuver:
Q1 0.05583000
ActNor.EstInrToBdy[0]
Q2 0.67101200
ActNor.EstInrToBdy[1]
Q3 0.21208700
ActNor.EstInrToBdy[2]
Q4 0.70826900
ActNor.EstInrToBdy[3]
MPS
Cmd Vector X 0.972761000
MPS
Cmd Vector Y 0.216101000
MPS
Cmd Vector Z 0.083887000
GPS sec 1270096268
ActNor.EstTime
UTC time 04/05/2020 04:30:54 output
CSS Angle TLM 0.148033
CSS Sun-Pointing Angle 0.296066
31 Mar 20 @ 13:00
CSS Angle TLM 0.260196
CSS Sun-Pointing Angle 0.520392
5 Apr 20 @ 4:30
Pre-Burn
Thruster 1 6608 31 Mar 20 @ 13:00
Thruster 2 6416
Thruster 3 8784
Thruster 4 8976
Post-Burn
Thruster 1 6848 5 Apr 20 @ 4:30
Thruster 2 6656
Thruster 3 9056
Thruster 4 9248
Number of Pulses
Thruster 1 240
Thruster 2 240
Thruster 3 272
Thruster 4 272
Thruster Pairs
Thruster 1 & 2 480
Thruster 3 & 4 544
Timothy E. Perry
Mission Operations
CRS, IBEX, OCO-2 & TESS
Office (703) 406-5976
Cell (301) 606-1430
