[Isocops] IBEX Goat Herder for 03 Feb 21

[Wesley, Sheral R [US] (SP)]

All,
The perigee contacts were nominal for CMD & TLM. The sun maneuver was successful.

Tasks Accomplished:

1.       Post Sun Maneuver :SetStaticZRate (estimator, 0.418)
StaticZRate @17:03:19z = 4.1653 RPM
StaticZRate @17:04:43z = 4.17699 RPM

2.       Reset FDC Totals: ResetTaskRawFailed (AC_FDC)

Results for the Sun Maneuver:
CSS Angle TLM  1.23638
CSS Sun-Pointing Angle 2.47276
29 Jan 21 @ 19:00:00

CSS Angle TLM  0.727124
CSS Sun-Pointing Angle 1.454248
03 Feb 21 @ 17:00:00

Pre-Burn
Thruster 1           1328       29 Jan 21 @ 19:00:00
Thruster 2           1280
Thruster 3           1568
Thruster 4           1616
Post-Burn
Thruster 1           1536       03 Feb 21 @ 17:00:00
Thruster 2           1488
Thruster 3           2000
Thruster 4           2048
Number of Pulses
Thruster 1           208
Thruster 2           208
Thruster 3           432
Thruster 4           432
Thruster Pairs
Thruster 1 & 2    416
Thruster 3 & 4    864

Sheral Wesley  |  Principal Engineer, Satellite Systems
Northrop Grumman Corporation  |  Space Systems
O: 703-406-5641  |  C: 202-236-0802  |  sheral.wesley at ngc.com<mailto:sheral.wesley at ngc.com>
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