[Isocops] IBEX Goat Herder for 11 Sept 20

[Perry, Timothy E [US] (IS)]

All,
   The apogee contact was nominal for CMD and TLM. The inertial maneuver was successful.

Results from the Inertial maneuver:
Q1 0.61936300 ActNor.EstInrToBdy[0]
Q2 -0.25912900 ActNor.EstInrToBdy[1]
Q3 -0.73023900 ActNor.EstInrToBdy[2]
Q4 0.12645800 ActNor.EstInrToBdy[3]

GPS sec 1283825098 ActNor.EstTime

UTC time 09/11/2020 02:04:44 output

MPS Diff 0.749 deg

MPS Cmd Vector X -0.971191000
MPS Cmd Vector Y 0.222433000
MPS Cmd Vector Z 0.085504000

CSS Angle TLM 0.304546
CSS Sun-Pointing Angle 0.609092
  06 Sept 20 @ 20:00:00

CSS Angle TLM 0.517377
CSS Sun-Pointing Angle 1.034754
  11 Sept 20 @ 02:00:00

Pre-Burn
Thruster 1 3600 06 Sept 20 @ 20:00:00
Thruster 2 3504
Thruster 3 4192
Thruster 4 4288
Post-Burn   `
Thruster 1 3872 11 Sept 20 @ 02:00:00
Thruster 2 3776
Thruster 3 4464
Thruster 4 4560
Number of Pulses
Thruster 1 272
Thruster 2 272
Thruster 3 272
Thruster 4 272
Thruster Pairs
Thruster 1 & 2 544
Thruster 3 & 4 544




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

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