[Isocops] IBEX Goat Herder for 6 July 22

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

All,
   The apogee contact was nominal and the inertial maneuver was successful.

Results from the Inertial Maneuver:
Q1 -0.30546800 ActNor.EstInrToBdy[0]
Q2 0.45864600 ActNor.EstInrToBdy[1]
Q3 0.77521800 ActNor.EstInrToBdy[2]
Q4 0.30882100 ActNor.EstInrToBdy[3]

GPS sec 1341143987 ActNor.EstTime

UTC time 07/06/2022 11:59:33 output
MPS Diff 0.852 deg
MPS Cmd Vector X -0.198474000
MPS Cmd Vector Y 0.903162000
MPS Cmd Vector Z 0.380667000
CSS Angle TLM 0.298707
CSS Sun-Pointing Angle 0.597414
  01 July 22 @10:00:00
CSS Angle TLM 0.3743
CSS Sun-Pointing Angle 0.7486
  06 July 22 @15:00:00
Pre-Burn
Thruster 1 1456 01 July 22 @10:00:00
Thruster 2 1424
Thruster 3 1872
Thruster 4 1904
Post-Burn
Thruster 1 1680 06 July 22 @15:00:00
Thruster 2 1648
Thruster 3 2128
Thruster 4 2160
Number of Pulses
Thruster 1 224
Thruster 2 224
Thruster 3 256
Thruster 4 256
Thruster Pairs
Thruster 1 & 2 448
Thruster 3 & 4 512


-------------- next part --------------
An HTML attachment was scrubbed...
URL: <https://lists.sr.unh.edu/pipermail/isocops/attachments/20220706/f2269f9b/attachment.html>