[Isocops] IBEX Goat Herder 10 and 11 June 2024

[Coca Gonzales, Andrea [US] (SP)]

Good morning team,

   The perigee contacts were nominal, and the inertial maneuver was successful. We performed the following, dump SSR (VCid2), and reset master timer. After the first 15 minutes of the second perigee pass, we switched to string 2 and sent a couple of commands and verified the telemetry points. Another mission took our support on DOY 180, so we did not upload the ATS since that contact has to be rescheduled first.

Tasks Accomplished:

Reset Master Timer
Reset FDC Totals
SSR Dump New (VCid2)

Results from the inertial maneuver:

Q1 -0.45830900
Q2 -0.31052300
Q3 -0.61640500
Q4 0.55997700

GPS sec 1402139230
UTC time 06/11/2024 11:06:56
MPS Diff 0.611

MPS Cmd Vector X 0.21003300
MPS Cmd Vector Y 0.90057100
MPS Cmd Vector Z 0.38060200

CSS Angle TLM 0.217606
CSS Sun-Pointing Angle 0.435212
  06 Jun 24 @12:00:00
CSS Angle TLM 0.251788
CSS Sun-Pointing Angle 0.503576
  11 Jun 24 @11:00:00

Pre-Burn
Thruster 1 26064 06 Jun 24 @12:00:00
Thruster 2 25312
Thruster 3 33920
Thruster 4 34672
Post-Burn
Thruster 1 26336 11 Jun 24 @11:00:00
Thruster 2 25584
Thruster 3 34192
Thruster 4 34944
Number of Pulses
Thruster 1 272
Thruster 2 272
Thruster 3 272
Thruster 4 272
Thruster Pairs
Thruster 1 & 2 544
Thruster 3 & 4 544

Kind regards,

Andrea Coca Gonzales | Associate Engineer Satellite Systems | MEV | ICESat-2 | TESS | IBEX
Northrop Grumman Corporation  |  Space Systems
C: 703-582-8233  |  Andrea.CocaGonzales at ngc.com<mailto:Andrea.CocaGonzales at ngc.com>

-------------- next part --------------
An HTML attachment was scrubbed...
URL: <https://lists.sr.unh.edu/pipermail/isocops/attachments/20240611/e8a14b74/attachment-0001.htm>