[Isocops] IBEX Goat Herder for 3 Nov 2024
Coca Gonzales, Andrea [US] (SP)
Andrea.CocaGonzales at ngc.com
Sun Nov 3 21:18:02 EST 2024
Good evening team,
The second perigee pass failed. SSC was having issues with the station and the station power was extremely low (between 11 and 34 watts throughout the pass). I switched to 2k and was able to get telemetry and make sure that the spacecraft itself was OK. I was also able to send a no-op. We'll need to schedule an extra support sometime this week to redump the missing blocks.
Best,
Andrea Coca Gonzales | Associate Engineer Satellite Systems | MEV | ICESat-2 | TESS | IBEX
Northrop Grumman Corporation | Dulles Chapter Adelante Member Engagement Lead | Space Systems
Andrea.CocaGonzales at ngc.com<mailto:Andrea.CocaGonzales at ngc.com>
From: Wesley, Sheral R [US] (SP) <Sheral.Wesley at ngc.com>
Sent: Sunday, November 3, 2024 10:56 AM
To: Coca Gonzales, Andrea [US] (SP) <Andrea.CocaGonzales at ngc.com>; bhautama at gmail.com; carol.weaver at unh.edu; Cavallo, John A [US] (SP) <John.Cavallo at ngc.com>; Chubin, Eric [US] (SP) <Eric.Chubin at ngc.com>; Fleming, Ed [US] (SP) <Ed.Fleming at ngc.com>; ADS-IBEX at l3harris.com; ibexops at gmail.com; IBEXOPS at gmail.com; isocops at lists.sr.unh.edu; kwfairchild at gmail.com; Ken.Fairchild at unh.edu; Leonard, Ben [US] (SP) <Benjamin.Leonard at ngc.com>; angoldconsulting at earthlink.net; nangold at princeton.edu; Perry, Timothy E [US] (SP) <Timothy.Perry at ngc.com>; Reed, Cheryl L [US] (SP) <Cheryl.Reed at ngc.com>; Tyler, Ryan S [US] (SP) <Ryan.Tyler at ngc.com>; Wynn, Reese [US] (SP) <Reese.Wynn at ngc.com>; ezirnstein at swri.edu; Wesley, Sheral R [US] (SP) <Sheral.Wesley at ngc.com>
Subject: IBEX Goat Herder for 3 Nov 2024
All,
The 1st perigee contact was intermittent for telemetry. The Orbit# 668 ATS was uploaded successfully, and the SSR_Dump will be re-dumped on the 2nd perigee contact
The following objectives were accomplished
1. Reset Master timer
2. SSR_Dump (new)
3. CAR# 1423 Upload Orbit# 668 ATS
IEBX_2024_318_o0688a_v001 (149-246)
Results from the inertial maneuver
Q1 0.56903700
Q2 -0.54756100
Q3 -0.10315900
Q4 0.60475700
GPS sec 1414675757
UTC time 11/03/2024 13:29:03
MPS Diff 0.738 deg
MPS Cmd Vector X -0.77535600
MPS Cmd Vector Y -0.57580900
MPS Cmd Vector Z -0.25935800
CSS Angle TLM 0.300296
CSS Sun-Pointing Angle 0.591491
30 Oct 24 @20:00:00
CSS Angle TLM 0.692386
CSS Sun-Pointing Angle 1.384772
03 Nov 24 @13:30:00
Pre-Burn
Thruster 1 8160 30 Oct 24 @20:00:00
Thruster 2 7952
Thruster 3 9696
Thruster 4 9904
Post-Burn
Thruster 1 8464 03 Nov 24 @13:30:00
Thruster 2 8256
Thruster 3 10000
Thruster 4 10208
Number of Pulses
Thruster 1 304
Thruster 2 304
Thruster 3 304
Thruster 4 304
Thruster Pairs
Thruster 1 & 2 608
Thruster 3 & 4 608
Best Regards,
Sheral Wesley | Sr Principal Engineer, Satellite Systems
Northrop Grumman Corporation | Space Systems
O: 703-406-5641 | C: 202-236-0802 | sheral.wesley at ngc.com<mailto:sheral.wesley at ngc.com>
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