[Isocops] Goat Herder for 1 March 2019

[Perry, Timothy]

All,

     The perigee contacts were nominal for CMD and TLM. The Inertial maneuver was successful.

The following was completed during these contacts:

Reset Master Timer

Set Spacecraft Clock

Reset FDC totals

SSR Dump _Dump New

FC Back Orbit dump

CAR 1025 ATS upload - IBEX _2019_069_o0440a_v001 - 81 cmds



Results from the Inertial maneuver:
Q1 -0.45747400 ActNor.EstInrToBdy[0]
Q2 0.59648600 ActNor.EstInrToBdy[1]
Q3 -0.54108800 ActNor.EstInrToBdy[2]
Q4 0.37702200 ActNor.EstInrToBdy[3]
GPS sec 1235435495.000 ActNor.EstTime
MPS Diff 0.707 deg
MPS Cmd Vector X 0.946998000
MPS Cmd Vector Y -0.290539000
MPS Cmd Vector Z -0.137047000
CSS Angle TLM 0.600357
CSS Sun-Pointing Angle 1.200714
  26 Feb 19 @18:00
CSS Angle TLM 0.479698
CSS Sun-Pointing Angle 0.959396
  01 Mar 19 @00:30
Pre-Burn
Thruster 1 6720 26 Feb 19 @18:00
Thruster 2 6576
Thruster 3 8112
Thruster 4 8256
Post-Burn
Thruster 1 6976 01 Mar 19 @00:30
Thruster 2 6832
Thruster 3 8384
Thruster 4 8528
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
RAPTOR Test Team
timothy.perry at ngc.com<mailto:timothy.perry at ngc.com>
Office (703) 406-5976
Cell (301) 606-1430

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