All,
The perigee passes were nominal
for CMD and TLM. The inertial maneuver was successful.
The following was accomplished:
Reset Master Timer
SSR Dump – Dump New
CAR # 1034 Dump Orbit 443 Missing blocks – All blocks were re-dumped with
no errors
CAR # 1035 Upload ATS Orbit # 446 IBEX_2019_124_o0446a_v001 91 cmds
Results from the Inertial maneuver:
Q1 0.12162500 ActNor.EstInrToBdy[0]
Q2 0.61390900 ActNor.EstInrToBdy[1]
Q3 0.51452300 ActNor.EstInrToBdy[2]
Q4 0.58616500 ActNor.EstInrToBdy[3]
GPS sec 1240257636.000 ActNor.EstTime
MPS Diff 0.795 deg
MPS Cmd Vector X 0.842741000
MPS Cmd Vector Y 0.497443000
MPS Cmd Vector Z 0.205760000
CSS Angle TLM 0.199851
CSS Sun-Pointing Angle 0.399702
20 Apr 19 @ 17:00
CSS Angle TLM 0.542846
CSS Sun-Pointing Angle 1.085692
25 Apr 19 @ 20:00
Pre-Burn
Thruster 1 9632 20 Apr 19 @ 17:00
Thruster 2 9408
Thruster 3 11792
Thruster 4 12016
Post-Burn
Thruster 1 9904 25 Apr 19 @ 20:00
Thruster 2 9680
Thruster 3 12080
Thruster 4 12304
Number of Pulses
Thruster 1 272
Thruster 2 272
Thruster 3 288
Thruster 4 288
Thruster Pairs
Thruster 1 & 2 544
Thruster 3 & 4 576
Timothy E. Perry
Mission Operations
CRS, IBEX, OCO-2 & TESS
RAPTOR Test Team
Office (703) 406-5976
Cell (301) 606-1430