All,
The first support was successful for CMD and TLM. Dumped the SSR and reset the Master Timer.
The Second support was not successful. We had another line outage. SSC was able to collect the VC0 data and brought up the carrier to get range data.
The ATS will be uplinked during the upcoming Apogee support. The Car for re-dumping the SSR data will be executed during next set of perigee supports. I was able to copy over the tlm files from SSC post pass and verify the Inertial maneuver.
The maneuver was successful and below are the maneuver results.
Q1 -0.52226300 ActNor.EstInrToBdy[0]
Q2 0.31083000 ActNor.EstInrToBdy[1]
Q3 0.78618900 ActNor.EstInrToBdy[2]
Q4 0.11194700 ActNor.EstInrToBdy[3]
GPS sec
1218312121.000 ActNor.EstTime
MPS Diff
0.661 deg
MPS Cmd Vector X -0.757047000
MPS Cmd Vector Y 0.603046000
MPS Cmd Vector Z 0.251427000
CSS Angle TLM 0.695207
CSS Sun-Pointing Angle 1.390414
10 Aug 18 @1130
CSS Angle TLM 1.41817
CSS Sun-Pointing Angle 2.83634
14 Aug 18 @1900
Pre-Burn
Thruster 1 3328 10 Aug 18 @1130
Thruster 2 3200
Thruster 3 3648
Thruster 4 3776
Post-Burn
Thruster 1 3600 14 Aug 18 @1900
Thruster 2 3472
Thruster 3 3952
Thruster 4 4080
Number of Pulses
Thruster 1 272
Thruster 2 272
Thruster 3 304
Thruster 4 304
Thruster Pairs
Thruster 1 & 2 544
Thruster 3 & 4 608
Timothy E. Perry
CRS, IBEX, OCO-2 & TESS
Mission Operations
Office (703) 406-5976
Cell (301) 606-1430
Corp Cell (571) 447-8977