All,
The perigee contact was nominal for CMD and TLM. The Inertial maneuver was successful. The Bus ATS for Orbit# 492 was uplinked. Stored Command count is at 216.
The following was accomplished:
CAR #2001 ATS upload – IBEX_2020_176_o0492a_BUS_V001 48 CMDS
Results for the Inertial maneuver:
Q1 -0.51258000
ActNor.EstInrToBdy[0]
Q2 -0.22654900
ActNor.EstInrToBdy[1]
Q3 -0.60121800
ActNor.EstInrToBdy[2]
Q4 0.56962600
ActNor.EstInrToBdy[3]
MPS
Cmd Vector X 0.351388000
MPS
Cmd Vector Y 0.862943000
MPS
Cmd Vector Z 0.363121000
GPS sec 1275130986
ActNor.EstTime
UTC time
06/02/2020 11:02:52 output
MPS Diff
0.738 deg
CSS Angle TLM 0.569926
CSS Sun-Pointing Angle 1.139852
29 May 20 @01:30
CSS Angle TLM 1.45804
CSS Sun-Pointing Angle 2.91608
02 May 20 @07:00
Pre-Burn
Thruster 1 9984 29 May 20 @01:30
Thruster 2 9712
Thruster 3 12640
Thruster 4 12912
Post-Burn
Thruster 1 10240 02 May 20 @07:00
Thruster 2 9968
Thruster 3 12912
Thruster 4 13184
Number of Pulses
Thruster 1 256
Thruster 2 256
Thruster 3 272
Thruster 4 272
Thruster Pairs
Thruster 1 & 2 512
Thruster 3 & 4 544
Timothy E. Perry
Mission Operations
CRS, IBEX, OCO-2
Office (703) 406-5976
Cell (301) 606-1430
