[Isocops] IBEX Goat Herder for 21 Aug 22

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

All,

    The spacecraft is nominal and the inertial maneuver was successful.  The STA spin rate looks valid. The rate changed from 4.177 to 4.181 post maneuver.



Results from the Inertial Maneuver:
Q1 0.24886700 ActNor.EstInrToBdy[0]
Q2 -0.56795000 ActNor.EstInrToBdy[1]
Q3 -0.65702200 ActNor.EstInrToBdy[2]
Q4 0.42874300 ActNor.EstInrToBdy[3]

GPS sec 1345082508 ActNor.EstTime
UTC time 08/21/2022 02:01:34 output

MPS Diff 0.631 deg

MPS Cmd Vector X -0.816774000
MPS Cmd Vector Y 0.533241000
MPS Cmd Vector Z 0.220306000

CSS Angle TLM 0.775817
CSS Sun-Pointing Angle 1.551634
  15 Aug 22 @16:30:00

CSS Angle TLM 0.527119
CSS Sun-Pointing Angle 1.054238
  21 Aug 22 @02:00:00

Pre-Burn
Thruster 1 4176 15 Aug 22 @16:30:00
Thruster 2 4080
Thruster 3 4720
Thruster 4 4816
Post-Burn
Thruster 1 4448 21 Aug 22 @02:00:00
Thruster 2 4352
Thruster 3 5040
Thruster 4 5136
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



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