All,
The first perigee contact was nominal for command/telemetry and the inertial maneuver was successful.
Tasks Accomplished:
- Reset master timer
- Reset FDC totals
- Set SC time
- Dump SSR (new)
- CAR# 1414 Orbit#663 HGC ATS Upload (875-938)
Results from the Inertial Maneuver:
Q1 -0.70390200
Q2 -0.10206800
Q3 0.69855100
Q4 0.07829600
GPS sec 1411484521
UTC time 09/27/2024 15:01:47
MPS Diff 0.717
MPS Cmd Vector X -0.99914900
MPS Cmd Vector Y -0.03337200
MPS Cmd Vector Z -0.02422300
CSS Angle TLM 0.866601
CSS Sun-Pointing Angle 1.733202
23 Sept 24 @23:30:00
CSS Angle TLM 0.117037
CSS Sun-Pointing Angle 0.234074
27 Sept 24 @14:00:00
Pre-Burn
Thruster 1 6128 23 Sept 24 @23:30:00
Thruster 2 5968
Thruster 3 6928
Thruster 4 7088
Post-Burn
Thruster 1 6432 27 Sept 24 @14:00:00
Thruster 2 6272
Thruster 3 7216
Thruster 4 7376
Number of Pulses
Thruster 1 304
Thruster 2 304
Thruster 3 288
Thruster 4 288
Thruster Pairs
Thruster 1 & 2 608
Thruster 3 & 4 576
Best Regards,
Sheral Wesley |
Sr
Principal Engineer, Satellite Systems
Northrop Grumman Corporation | Space Systems
O: 703-406-5641 | C: 202-236-0802 |
sheral.wesley@ngc.com
From: Perry, Timothy E [US] (SP) <Timothy.Perry@ngc.com>
Sent: Monday, September 23, 2024 8:09 PM
To: bhautama@gmail.com; carol.weaver@unh.edu; Cavallo, John A [US] (SP) <John.Cavallo@ngc.com>; Chubin, Eric [US] (SP) <Eric.Chubin@ngc.com>; Coca Gonzales, Andrea [US] (SP) <Andrea.CocaGonzales@ngc.com>; Fleming, Ed [US] (SP) <Ed.Fleming@ngc.com>; ADS-IBEX@l3harris.com;
ibexops@gmail.com; IBEXOPS@gmail.com; isocops@lists.sr.unh.edu; kwfairchild@gmail.com; Ken.Fairchild@unh.edu; Leonard, Ben [US] (SP) <Benjamin.Leonard@ngc.com>; angoldconsulting@earthlink.net; nangold@princeton.edu; Perry, Timothy E [US] (SP) <Timothy.Perry@ngc.com>;
Reed, Cheryl L [US] (SP) <Cheryl.Reed@ngc.com>; Tyler, Ryan S [US] (SP) <Ryan.Tyler@ngc.com>; Wesley, Sheral R [US] (SP) <Sheral.Wesley@ngc.com>; Wynn, Reese [US] (SP) <Reese.Wynn@ngc.com>; ezirnstein@swri.edu
Subject: IBEX Goat Herder for 23 Sept 2024
All,
The apogee contact was nominal. The inertial maneuver was successful.
Tasks Accomplished:
Reset FDC totals
Results from the Inertial Maneuver:
Q1 0.69799500 ActNor.EstInrToBdy[0]
Q2 -0.04554130 ActNor.EstInrToBdy[1]
Q3 -0.71443000 ActNor.EstInrToBdy[2]
Q4 0.01786840 ActNor.EstInrToBdy[3]
GPS sec 1411169500 ActNor.EstTime
UTC time
09/23/2024 23:31:26 output
MPS Diff
0.844 deg
MPS Cmd Vector X -0.99918000
MPS Cmd Vector Y 0.03992200
MPS Cmd Vector Z 0.00673700
CSS Angle TLM 1.30409
CSS Sun-Pointing Angle 2.60818
18 Sept 24 @07:00:00
CSS Angle TLM 0.866601
CSS Sun-Pointing Angle 1.733202
23 Sept 24 @23:30:00
Pre-Burn
Thruster 1 6000 18 Sept 24 @07:00:00
Thruster 2 5840
Thruster 3 6784
Thruster 4 6944
Post-Burn
Thruster 1 6128 23 Sept 24 @23:30:00
Thruster 2 5968
Thruster 3 6928
Thruster 4 7088
Number of Pulses
Thruster 1 128
Thruster 2 128
Thruster 3 144
Thruster 4 144
Thruster Pairs
Thruster 1 & 2 256
Thruster 3 & 4 288
Timothy E.Perry
CRS IBEX OCO-2
Mission Operations
Office (703) 406-5976
Cell (301) 606-1430