All,
The contact was nominal for CMD and TLM. The Star tracker went thru an autonomous reset in the back orbit. The star tracker was nominal at AOS. I executed Standing CAR # 344 Reset FDC Totals
and Response latch values. I will get the time of the reset after the SSR dump on DOY 140. The Inertial maneuver as successful. The Bus ATS for Orbit 490 was uplinked.
The following was accomplished:
CAR #344 - Reset FDC Totals and Response latch values
CAR #1098 – ATS upload – IBEX_2020_158_o0490a_BUS_V001 46
cmds
Results from the Inertial maneuver:
Q1 0.11002800
ActNor.EstInrToBdy[0]
Q2 0.57495900
ActNor.EstInrToBdy[1]
Q3 0.70696500
ActNor.EstInrToBdy[2]
Q4 0.39663200
ActNor.EstInrToBdy[3]
GPS sec 1273579652
ActNor.EstTime
MPS Diff 0.577
deg
MPS
Cmd Vector X 0.612832000
MPS
Cmd Vector Y 0.728974000
MPS
Cmd Vector Z 0.305014000
CSS Angle TLM 0.359909
CSS Sun-Pointing Angle 0.719818
11 May 20 @ 00:30
CSS Angle TLM 1.12917
CSS Sun-Pointing Angle 2.25834
15 May 20 @12:00
Pre-Burn
Thruster 1 8928 11 May 20 @ 00:30
Thruster 2 8656
Thruster 3 11488
Thruster 4 11760
Post-Burn
Thruster 1 9200 15 May 20 @12:00
Thruster 2 8928
Thruster 3 11808
Thruster 4 12080
Number of Pulses
Thruster 1 272
Thruster 2 272
Thruster 3 320
Thruster 4 320
Thruster Pairs
Thruster 1 & 2 544
Thruster 3 & 4 640
Timothy E. Perry
Mission Operations
CRS, IBEX, OCO-2 & TESS
Office (703) 406-5976
Cell (301) 606-1430
