All,

The 2 perigee SSC supports were nominal for CMD and TLM. The Inertial maneuver was successful.

I will check with APL in the morning for the SSR dump files.

The following was accomplished:

Reset FDC totals

Reset Master Timer

CAR #1047 ATS Upload – IBEX_2019_197_o0454a_V001 93 Cmds

Results from the Inertial maneuver:

Q1 -0.20741000 ActNor.EstInrToBdy[0]

Q2 -0.51200800 ActNor.EstInrToBdy[1]

Q3 -0.68047200 ActNor.EstInrToBdy[2]

Q4 0.48144300 ActNor.EstInrToBdy[3]

GPS sec 1246516283 ActNor.EstTime

UTC time 07/07/2019 06:31:09 output

MPS Diff 0.686 deg

MPS Cmd Vector X -0.217197000

MPS Cmd Vector Y 0.899157000

MPS Cmd Vector Z 0.379924000

CSS Angle TLM 0.173589

CSS Sun-Pointing Angle 0.347178

02 July 19 @ 13:00

CSS Angle TLM 0

CSS Sun-Pointing Angle 0

07 July 19 @ 06:30

Pre-Burn

Thruster 1 13952 02 July 19 @ 13:00

Thruster 2 13632

Thruster 3 16496

Thruster 4 16816

Post-Burn

Thruster 1 14288 07 July 19 @ 06:30

Thruster 2 13904

Thruster 3 16800

Thruster 4 17184

Number of Pulses

Thruster 1 336

Thruster 2 272

Thruster 3 304

Thruster 4 368

Thruster Pairs

Thruster 1 & 2 608

Thruster 3 & 4 672

Timothy E. Perry

Mission Operations

CRS, IBEX, OCO-2 & TESS

timothy.perry@ngc.com

Office (703) 406-5976

Cell (301) 606-1430

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