All,
The Perigee contacts were nominal for command and telemetry. The sun maneuver was successful.
Tasks Accomplished:
On both perigee contacts - SSR Dump à Dump New
Dump back-orbit buffer
CAR #1276 Orbit 588 ATS Upload
IBEX_2022_320_o0588a_v001.scr 88 cmds
Reset Master 18 day Timer
Set Spacecraft Clock
Reset AC/FDC failed totals
Results from the Sun Maneuver
CSS Angle TLM 1.96394
CSS Sun-Pointing Angle 3.92788
05 Nov 22@03:30:00
CSS Angle TLM 1.3106
CSS Sun-Pointing Angle 2.6212
07 Nov 22@11:00:00
Pre-Burn
Thruster 1 8400 05 Nov 22@03:30:00
Thruster 2 8160
Thruster 3 10864
Thruster 4 11104
Post-Burn
Thruster 1 8576 07 Nov 22@11:00:00
Thruster 2 8288
Thruster 3 11280
Thruster 4 11568
Number of Pulses
Thruster 1 176
Thruster 2 128
Thruster 3 416
Thruster 4 464
Thruster Pairs
Thruster 1 & 2 304
Thruster 3 & 4 880
Eric Chubin | Principal Engineer Satellite Systems
Northrop Grumman Corporation | Space Systems