[Isocops] IBEX Goat Herder for Feb 16 2020

[Chubin, Eric [US] (IS)]

All,

The Apogee pass was nominal for CMD and TLM. The Inertial maneuver was successful.

Results from the Inertial Maneuver:


Q1 -0.63168700 ActNor.EstInrToBdy[0]
Q2 0.45750000  ActNor.EstInrToBdy[1]
Q3 -0.62315400 ActNor.EstInrToBdy[2]
Q4 0.05782350  ActNor.EstInrToBdy[3]

GPS sec 1265907562 ActNor.EstTime

UTC time 02/16/2020 16:59:08
MPS Diff 0.480 deg
MPS Cmd Vector X 0.841256000
MPS Cmd Vector Y -0.492320000
MPS Cmd Vector Z -0.223403000
CSS Angle TLM   1.378
CSS Sun-Pointing Angle   2.756
10 Feb 20 @ 23:30
CSS Angle TLM   1.137
CSS Sun-Pointing Angle   2.274
16 Feb 20 @ 17:00
Pre-Burn
Thruster 1 4016  10 Feb 20 @ 23:30
Thruster 2 3872
Thruster 3 5440
Thruster 4 5584
Post-Burn
Thruster 1 4272  16 Feb 20 @ 17:00
Thruster 2 4128
Thruster 3 5744
Thruster 4 5888
Number of Pulses
Thruster 1 256
Thruster 2 256
Thruster 3 304
Thruster 4 304
Thruster Pairs
Thruster 1 & 2    512
Thruster 3 & 4    608




Eric Chubin  |  Engineer Systems
Northrop Grumman Corporation  |  Space Systems
O: 703-429-7015  |  C: 240-328-2098  |  eric.chubin at ngc.com

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