All,
The Apogee contact was nominal for CMD and TLM. The Inertial maneuver was successful. .
Results of the maneuver:
0.70736200 ActNor.EstInrToBdy[0]
-0.43421500 ActNor.EstInrToBdy[1]
0.10898200 ActNor.EstInrToBdy[2]
0.54700900 ActNor.EstInrToBdy[3]
1228222842.000
ActNor.EstTime
MPS Cmd Vector X -0.317803000
MPS Cmd Vector Y -0.865955000
MPS Cmd Vector Z -0.386164000
MPS Diff
0.532 deg
CSS Angle TLM 0.483355
CSS Sun-Pointing Angle 0.96671
29 Nov 18 @19:30
CSS Angle TLM 0.97438
CSS Sun-Pointing Angle 1.94876
7 Dec 18 @13:00
Pre-Burn
Thruster 1 1392 29 Nov 18 @19:30
Thruster 2 1392
Thruster 3 1504
Thruster 4 1504
Post-Burn
Thruster 1 1856 7 Dec 18 @13:00
Thruster 2 1808
Thruster 3 1952
Thruster 4 2000
Number of Pulses
Thruster 1 464
Thruster 2 416
Thruster 3 448
Thruster 4 496
Thruster Pairs
Thruster 1 & 2 880
Thruster 3 & 4 944
Timothy E. Perry
Mission Operations
CRS, IBEX, OCO-2 & TESS
RAPTOR Test Team
timothy.perry@ngc.com
Office (703) 406-5976
Cell (301) 606-1430

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