All,
The perigee contacts were nominal for CMD and TLM. The Inertial maneuver was successful. The
SSR dump was successful during the first contact. I also dumped the SSR during the second contact. The Instrument ATS for Orbit 498 was uplinked. 18 Day timer command executed and counter was reset to 10. Deleted stored commands for APL and the SSC contact
on 08/09/2020@19:00gmt.
Tasks Accomplished:
CAR #1106 ATS upload
IBEX_2020_232_o0498a_INST_V001 46
cmds
SSR Dump -> Dump New (2ea)
Set Spacecraft Clock
Deleted Timed commands for APL and original SSC contact. on 08/09/2020@19:00gmt
Results for the Inertial maneuver:
Q1 -0.47604600
ActNor.EstInrToBdy[0]
Q2 -0.36396800
ActNor.EstInrToBdy[1]
Q3 0.13841600
ActNor.EstInrToBdy[2]
Q4 0.78851100
ActNor.EstInrToBdy[3]
GPS sec 1281031399
ActNor.EstTime
UTC time 08/09/2020 18:03:05 output
MPS Diff 0.511
deg
MPS
Cmd Vector X -0.705841000
MPS
Cmd Vector Y 0.653433000
MPS
Cmd Vector Z 0.273523000
CSS Angle TLM 0.77718
CSS Sun-Pointing Angle 1.55436
5 Aug 20 @ 11:00
CSS Angle TLM 0.239031
CSS Sun-Pointing Angle 0.478062
9 Aug 20 @ 17:00
Pre-Burn
Thruster 1 1712 5 Aug 20 @ 11:00
Thruster 2 1680
Thruster 3 2000
Thruster 4 2032
Post-Burn
`
Thruster 1 2000 9 Aug 20 @ 17:00
Thruster 2 1936
Thruster 3 2304
Thruster 4 2368
Number of Pulses
Thruster 1 288
Thruster 2 256
Thruster 3 304
Thruster 4 336
Thruster Pairs
Thruster 1 & 2 544
Thruster 3 & 4 640
Timothy E. Perry
Mission Operations
CRS, IBEX, OCO-2
Office (703) 406-5976
Cell (301) 606-1430
