[Isocops] IBEX Goat Herder for Aug 11 & 12

[Perry, Timothy]

All,

    The perigee passes were nominal for CMD & TLM. The Inertial maneuver was successful.

For this orbit we had 2 star tracker resets. The first was on DOY 218/07:41:58 (Razor Issue I100-657) and the second was on DOY 224/11:19:51 (Razor Issue I100-658).

Both times the star tracker recovered normally and CAR 344 was used to reset the error flags.



The following was completed:

Reset the master Timer

SSR Dump -> Dump New

Dump FCBO buffer

CAR # 1053 ATS upload - IBEX_2019_233_o0458a_V001 91 Cmds

Set SC Time

Results from the Inertial maneuver:
Q1 -0.60136100 ActNor.EstInrToBdy[0]
Q2 0.01962110 ActNor.EstInrToBdy[1]
Q3 0.61926600 ActNor.EstInrToBdy[2]
Q4 0.50447000 ActNor.EstInrToBdy[3]
GPS sec 1249653965 ActNor.EstTime
UTC time 08/12/2019 14:05:51 output
MPS Diff 0.701 deg
MPS Cmd Vector X -0.728296000
MPS Cmd Vector Y 0.632273000
MPS Cmd Vector Z 0.264227000
CSS Angle TLM 1.81951
CSS Sun-Pointing Angle 3.63902
  07 Aug 19 @ 12:00
CSS Angle TLM 0.815654
CSS Sun-Pointing Angle 1.631308
  12 Aug 19 @ 14:00
Pre-Burn
Thruster 1 15952 07 Aug 19 @ 12:00
Thruster 2 15568
Thruster 3 18944
Thruster 4 19328
Post-Burn
Thruster 1 16208 12 Aug 19 @ 14:00
Thruster 2 15824
Thruster 3 19216
Thruster 4 19600
Number of Pulses
Thruster 1 256
Thruster 2 256
Thruster 3 272
Thruster 4 272
Thruster Pairs
Thruster 1 & 2 512
Thruster 3 & 4 544



Timothy E. Perry
Mission Operations
CRS, IBEX, OCO-2 & TESS
timothy.perry at ngc.com<mailto:timothy.perry at ngc.com>
Office (703) 406-5976
Cell (301) 606-1430

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