All,
The perigee contacts were nominal for CMD and TLM. The inertial maneuver was successful. The master timer reset command executed and was verified. The Time for the Star tracker reset was 23 May2020 @09:17:24z
The following was accomplished:
SSR Dump -> Dump New
CAR #1098 ATS Upload – IBEX_2020_158_o0490a_INST_v001
Results from the inertial maneuver:
Q1 -0.33070100
ActNor.EstInrToBdy[0]
Q2 -0.45833700
ActNor.EstInrToBdy[1]
Q3 -0.81562000
ActNor.EstInrToBdy[2]
Q4 0.12380300
ActNor.EstInrToBdy[3]
MPS
Cmd Vector X 0.418853000
MPS
Cmd Vector Y 0.836686000
MPS
Cmd Vector Z 0.352871000
GPS sec 1274751813
ActNor.EstTime
UTC time 05/29/2020 01:43:19 output
MPS Diff 0.748
deg
CSS Angle TLM 0.5203
CSS Sun-Pointing Angle 1.0406
24 May 20 @12:00
CSS Angle TLM 0.569926
CSS Sun-Pointing Angle 1.139852
29 May 20 @01:30
Pre-Burn
Thruster 1 9712 24 May 20 @12:00
Thruster 2 9440
Thruster 3 12352
Thruster 4 12624
Post-Burn
Thruster 1 9984 29 May 20 @01:30
Thruster 2 9712
Thruster 3 12640
Thruster 4 12912
Number of Pulses
Thruster 1 272
Thruster 2 272
Thruster 3 288
Thruster 4 288
Thruster Pairs
Thruster 1 & 2 544
Thruster 3 & 4 576
Timothy E. Perry
Mission Operations
CRS, IBEX, OCO-2
Office (703) 406-5976
Cell (301) 606-1430
