All,
The apogee pass was nominal for CMD and TLM. The Inertial maneuver was successful.
Results from the maneuver:
Q1 0.46650400
ActNor.EstInrToBdy[0]
Q2 0.40276100
ActNor.EstInrToBdy[1]
Q3 0.78242200
ActNor.EstInrToBdy[2]
Q4 0.08929270
ActNor.EstInrToBdy[3]
GPS sec 1240595914.000
ActNor.EstTime
MPS Diff 0.802
deg
MPS Cmd Vector X 0.799100000
MPS Cmd Vector Y 0.555575000
MPS Cmd Vector Z 0.229727000
CSS Angle TLM 0.542846
CSS Sun-Pointing Angle 1.085692
25 Apr 19 @ 20:00
CSS Angle TLM 0.355533
CSS Sun-Pointing Angle 0.711066
29 Apr 19 @ 18:00
Pre-Burn
Thruster 1 9904 25 Apr 19 @ 20:00
Thruster 2 9680
Thruster 3 12080
Thruster 4 12304
Post-Burn
Thruster 1 10192 29 Apr 19 @ 18:00
Thruster 2 9936
Thruster 3 12384
Thruster 4 12640
Number of Pulses
Thruster 1 288
Thruster 2 256
Thruster 3 304
Thruster 4 336
Thruster Pairs
Thruster 1 & 2 544
Thruster 3 & 4 640
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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