All,
The perigee passes were nominal for CMD and TLM. The Inertial maneuver was successful.
We completed the following:
SSR Dump -> Dump New
CAR #1040 Dump Orbit #448 Missing blocks
CAR #1041 ATS upload – IBEX_2019_170_o0451a_v001
Reset Master Timer
Set Spacecraft Clock
Result from the Inertial maneuver:
Q1 -0.34657700
ActNor.EstInrToBdy[0]
Q2 -0.43152700
ActNor.EstInrToBdy[1]
Q3 -0.76186200
ActNor.EstInrToBdy[2]
Q4 0.33650500
ActNor.EstInrToBdy[3]
GPS sec 1244220803.000
ActNor.EstTime
MPS Diff 0.707
deg
MPS Cmd Vector X 0.230781000
MPS Cmd Vector Y 0.896300000
MPS Cmd Vector Z 0.378665000
CSS Angle TLM 0.668811
CSS Sun-Pointing Angle 1.337622
5
June 19 @ 13:00
CSS Angle TLM 0.859118
CSS Sun-Pointing Angle 1.718236
10 June 19 @ 02:00
Pre-Burn
Thruster 1 12368 5
June 19 @ 13:00
Thruster 2 12048
Thruster 3 14768
Thruster 4 15088
Post-Burn
Thruster 1 12640 10 June 19 @ 02:00
Thruster 2 12320
Thruster 3 15072
Thruster 4 15392
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
Mission Operations
CRS, IBEX, OCO-2 & TESS
RAPTOR Test Team
Office (703) 406-5976
Cell (301) 606-1430