All,
The perigee contacts were successful for CMD and TLM. The second contact had uplink issues at the beginning of the contact. The reason for the issue is still under investigation. The Inertial maneuver was successful.
The following commanding was completed:
Reset Master Timer
SSR Dump -> Dump new and reset the pointers to 70000
CAR #1042 IBEX Hi Background test and Lo magneto tail Season
Completed Pass #2 – Upload Hi Normal and Lo Magneto tail sweep tables.
CAR #1046 upload ATS Orbit #453
IBEX_2019_188_o0453a_V001 93 Cmds
CAR #1044 upload ATS Orbit #452 APL contact
IBEX_2019_o0452a_APL18_V001 6 Cmds
CAR #1045 upload ATS Orbit #453 APL contact
IBEX_2019_o0453a_APL18_V001 7 Cmds
Results
frm the maneuver:
Q1 -0.53781400
ActNor.EstInrToBdy[0]
Q2 0.11095200
ActNor.EstInrToBdy[1]
Q3 0.22708700
ActNor.EstInrToBdy[2]
Q4 0.80428600
ActNor.EstInrToBdy[3]
GPS sec 1245783798
ActNor.EstTime
MPS Diff 0.524
deg
MPS Cmd Vector X -0.066571000
MPS Cmd Vector Y 0.919042000
MPS Cmd Vector Z 0.388497000
CSS Angle TLM 0.737544
CSS Sun-Pointing Angle 1.475088
24 June 19 @ 13:00
CSS Angle TLM 1.26594
CSS Sun-Pointing Angle 2.53188
28 June 19 @ 03:00
Pre-Burn
Thruster 1 13424 24 June 19 @ 13:00
Thruster 2 13104
Thruster 3 15920
Thruster 4 16240
Post-Burn
Thruster 1 13696 28 June 19 @ 03:00
Thruster 2 13376
Thruster 3 16224
Thruster 4 16544
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
Office (703) 406-5976
Cell (301) 606-1430