All,
The Apogee contact was nominal for CMD and TLM. The inertial maneuver was successful.
Tim
Q1 -0.24930800
ActNor.EstInrToBdy[0]
Q2 0.69745300
ActNor.EstInrToBdy[1]
Q3 -0.36248800
ActNor.EstInrToBdy[2]
Q4 0.56569200
ActNor.EstInrToBdy[3]
GPS sec
1236110415.000 ActNor.EstTime
MPS Diff
0.519 deg
MPS Cmd Vector X 0.969799000
MPS Cmd Vector Y -0.219924000
MPS Cmd Vector Z -0.105466000
CSS Sun-Pointing Angle 0.959396
01 Mar 19 @00:30
CSS Angle TLM 0.206534
CSS Sun-Pointing Angle 0.413068
08 Mar 19 @20:00
Pre-Burn
Thruster 1 6976 01 Mar 19 @00:30
Thruster 2 6832
Thruster 3 8384
Thruster 4 8528
Post-Burn
Thruster 1 7296 08 Mar 19 @20:00
Thruster 2 7120
Thruster 3 8720
Thruster 4 8896
Number of Pulses
Thruster 1 320
Thruster 2 288
Thruster 3 336
Thruster 4 368
Thruster Pairs
Thruster 1 & 2 608
Thruster 3 & 4 704
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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