All,

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

The following was completed:

CAR# 1003 ATS Uplink “IBEX_2018_316_o0427a_v001” 93 cmds

Dump the FC Back orbit data

SSR Dump

Reset the master reset timer

Reset FDC Totals

Set the SC clock

Maneuver Results:

Q1 -0.58956500 ActNor.EstInrToBdy[0]

Q2 -0.52376800 ActNor.EstInrToBdy[1]

Q3 0.61150600 ActNor.EstInrToBdy[2]

Q4 0.06433740 ActNor.EstInrToBdy[3]

GPS sec 1225288915.000 ActNor.EstTime

MPS Cmd Vector X -0.785543000

MPS Cmd Vector Y -0.564034000

MPS Cmd Vector Z -0.254534000

MPS Diff 0.637

CSS Angle TLM 1.95805

CSS Sun-Pointing Angle 3.9161

29 Oct 18 @ 23:00

CSS Angle TLM 0.604579

CSS Sun-Pointing Angle 1.209158

03 NOv 18 @ 14:00

Pre-Burn

Thruster 1 8176 29 Oct 18 @ 23:00

Thruster 2 7936

Thruster 3 9072

Thruster 4 9312

Post-Burn

Thruster 1 8448 03 NOv 18 @ 14:00

Thruster 2 8208

Thruster 3 9360

Thruster 4 9600

Number of Pulses

Thruster 1 272

Thruster 2 272

Thruster 3 288

Thruster 4 288

Thruster Pairs

Thruster 1 & 2 544

Thruster 3 & 4 576

Timothy E. Perry

Mission Operations

CRS, IBEX, OCO-2 & TESS

RAPTOR Test Team

Tim.perry@ngc.com

Office (703) 406-5976

Cell (301) 606-1430

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