All,
The apogee contact was nominal for CMD and TLM. The Inertial maneuver was successful.
The ATS for Orbit# 429 was uplinked:
CAR 1007 - ATS upload – IBEX _2018_334_o0429a_v001
Q1 0.50876300 ActNor.EstInrToBdy[0]
Q2 0.64308400 ActNor.EstInrToBdy[1]
Q3 -0.56863800 ActNor.EstInrToBdy[2]
Q4 0.06521770 ActNor.EstInrToBdy[3]
GPS sec
1227396685.000 ActNor.EstTime
MPS Cmd Vector X -0.490666000
MPS Cmd Vector Y -0.795325000
MPS Cmd Vector Z -0.355955000
MPS Diff
0.697 deg
CSS Angle TLM 1.35595
CSS Sun-Pointing Angle 2.7119
20 Nov 18 @ 18:00
CSS Angle TLM 1.70949
CSS Sun-Pointing Angle 3.41898
27 Nov 18 @23:30
Pre-Burn
Thruster 1 816 20 Nov 18 @ 18:00
Thruster 2 816
Thruster 3 896
Thruster 4 896
Post-Burn
Thruster 1 1120 27 Nov 18 @23:30
Thruster 2 1120
Thruster 3 1200
Thruster 4 1200
Number of Pulses
Thruster 1 304
Thruster 2 304
Thruster 3 304
Thruster 4 304
Thruster Pairs
Thruster 1 & 2 608
Thruster 3 & 4 608
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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