All,
The Apogee passes were nominal. Collected CSS data and sent it off to Bret and Ryan. It seems that the difference between the old CEU default spin pulse and the new was only a value of 1 (Old 57359, New 57358). I did not update the
spin pulse value during the second since it was so close to the second one. We did achieve 40k during the support. CAR 853 Dump Orbit 327 missing blocks was executed and 40 blocks with no errors. The maneuver looked nominal. Below are values for the post maneuver
checks:
Q1 -0.47298800 ActNor.EstInrToBdy[0]
Q2 -0.30484300 ActNor.EstInrToBdy[1]
Q3 -0.69214600 ActNor.EstInrToBdy[2]
Q4 0.45198200 ActNor.EstInrToBdy[3]
GPS sec 1148730000.000 ActNor.EstTime
MPS Diff
0.517
MPS Cmd Vector X
0.377391000
MPS Cmd Vector Y
0.853683000
MPS Cmd Vector Z
0.358889000
26 May 16 @2330
CSS Angle TLM 1.44021
CSS Sun-Pointing Angle 2.88042
31 May 16 @1200
CSS Angle TLM 1.376
CSS Sun-Pointing Angle 2.752
Pre-Burn
Thruster 1 12224 26 May 16 @2330
Thruster 2 11824
Thruster 3 16160
Thruster 4 16560
Post-Burn
Thruster 1 12400 31 May 16 @1200
Thruster 2 12000
Thruster 3 16368
Thruster 4 16768
Number of Pulses
Thruster 1 176
Thruster 2 176
Thruster 3 208
Thruster 4 208
Thruster Pairs
Thruster 1 & 2 352
Thruster 3 & 4 416
Timothy E.Perry
CRS, IBEX & OCO-2
Mission Operations
tim.perry@orbitalatk.com
Office (703) 406-5976
Cell (301) 606-1430
Corp Cell (571)-447-8977