All,
The perigee contacts were nominal. The Inertial maneuver was successful. During the second pass we were able to use the maestro1 string. We performed the
following, dump SSR( VCid2), Dump Flight computer back orbit data(VCid1) and reset master timer.
Tasks Accomplished:
Reset Master Timer
Reset FDC Totals
SSR Dump -> Dump New
Dumped FC Back Orbit Data
CAR #1384 Orbit 645 ATS upload
IBEX_2024_108_o0645a_v001 111 commands
Results from the Inertial Maneuver
Q1 -0.22002900 ActNor.EstInrToBdy[0]
Q2 0.62952300 ActNor.EstInrToBdy[1]
Q3 -0.05519020 ActNor.EstInrToBdy[2]
Q4 0.74313000 ActNor.EstInrToBdy[3]
GPS sec 1396600297 ActNor.EstTime
UTC time
04/08/2024 08:31:23 output
MPS Diff
0.608 deg
MPS Cmd Vector X 0.95792600
MPS Cmd Vector Y 0.266791000
MPS Cmd Vector Z 0.105830000
CSS Angle TLM 0.413068
CSS Sun-Pointing Angle 0.826136
04 Apr 24 @13:00:00
CSS Angle TLM 0.413068
CSS Sun-Pointing Angle 0.826136
08 Apr 24 @08:30:00
Pre-Burn
Thruster 1 22224 04 Apr 24 @13:00:00
Thruster 2 21568
Thruster 3 29744
Thruster 4 30400
Post-Burn
Thruster 1 22496 08 Apr 24 @08:30:00
Thruster 2 21840
Thruster 3 30048
Thruster 4 30704
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
Mission Operations
Office (703) 406-5976
IBEX MOC (703)404-7470
Cell (301) 606-1430