All,
The Support was nominal for CMD and TLM. The Inertial maneuver was nominal.
Results for the Inertial maneuver:
Q1 -0.50458100
ActNor.EstInrToBdy[0]
Q2 0.32134400
ActNor.EstInrToBdy[1]
Q3 -0.19609500
ActNor.EstInrToBdy[2]
Q4 0.77697100
ActNor.EstInrToBdy[3]
GPS sec
1241442149.000 ActNor.EstTime
UTC time
05/09/2019 13:02:15 output
MPS Diff
0.537 deg
MPS Cmd Vector X 0.696203000
MPS Cmd Vector Y 0.662614000
MPS Cmd Vector Z 0.276124000
CSS Angle TLM 0.739134
CSS Sun-Pointing Angle 1.478268
04 May 19 @ 22:00
CSS Angle TLM 0.862981
CSS Sun-Pointing Angle 1.725962
09 May 19 @ 13:00
Pre-Burn
Thruster 1 10464 04 May 19 @ 22:00
Thruster 2 10205
Thruster 3 12688
Thruster 4 12944
Post-Burn
Thruster 1 10736 09 May 19 @ 13:00
Thruster 2 10480
Thruster 3 12992
Thruster 4 13248
Number of Pulses
Thruster 1 272
Thruster 2 275
Thruster 3 304
Thruster 4 304
Thruster Pairs
Thruster 1 & 2 547
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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