[Isocops] IBEX Goat Herder for 26 Oct 23

NIgel Angold nangold at princeton.edu
Thu Oct 26 19:09:47 EDT 2023


Thank you for extending the contact to get things done.

Nigel
> Wesley, Sheral R [US] (SP) <mailto:Sheral.Wesley at ngc.com>
> October 26, 2023 at 17:41
>
> All,
>
>     The perigee contacts were nominal. The sun maneuver was 
> successful. The current star percent valid is at 79%.
>
> The following contact was extended to successfully re-dump Orbit 624 
> VC2 data
>
>   IBEX,AUWA01,ADD,10/26/23,299,20:00:00,10/26/23,299,21:30:00,LAHO 64K 
> IBEX-3 Orbit# 625 Tracking Contact 11re Perigee
>
> Tasks Accomplished:
>
> Reset Master Timer
>
> SSR Dump -> Dump New (4136 est. remaining blocks)
>
> Set Static Z rate
>
> CAR# 1349 Upload Orbit# 626 (26 Oct – 4 Nov 23)
>
> IBEX_2023_299_o0626a_v001.scr (753-855)
>
> CAR# 1350 Upload Orbit# 627 (4 Nov – 13 Nov 23)
>
> IBEX_2023_308_o0627a_v002.scr (856-953)
>
> CAR# 1348 Redump orbit# 624 Blocks (SSR Dump.scr, Start 123010, 
> Numblks, 29740)
>
> Results from the Sun Maneuver:
>
> CSS Angle TLM   0.976787
>
> CSS Sun-Pointing Angle  1.953574
>
>                                 25 Oct 23 at 01:00:00
>
> CSS Angle TLM   1.64746
>
> CSS Sun-Pointing Angle  3.29492
>
>                                 26 Oct 23 at 11:15:00
>
> Pre-Burn
>
> Thruster 1           13440   25 Oct 23 at 01:00:00
>
> Thruster 2           13072
>
> Thruster 3           17328
>
> Thruster 4           17696
>
> Post-Burn
>
> Thruster 1           13632   26 Oct 23 at 11:15:00
>
> Thruster 2           13216
>
> Thruster 3           17760
>
> Thruster 4           18176
>
> Number of Pulses
>
> Thruster 1           192
>
> Thruster 2           144
>
> Thruster 3           432
>
> Thruster 4           480
>
> Thruster Pairs
>
> Thruster 1 & 2   336
>
> Thruster 3 & 4   912
>
> Best Regards,
>
> **
>
> *Sheral*Wesley  |SrPrincipal 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>
>
> Perry, Timothy E [US] (SP) <mailto:Timothy.Perry at ngc.com>
> October 24, 2023 at 21:41
>
> All,
>
>     The apogee contact was nominal. The sun maneuver was successful. 
> The static Z rate was set during the contact. The current star percent 
> valid is at 72%.
>
> Tasks Accomplished:
>
> Reset FDC Totals
>
> Set Static Z rate
>
> Results from the Sun Maneuver:
>
> CSS Angle TLM 0.832748
>
> CSS Sun-Pointing Angle 1.665496
>
>   17 Oct 23 at 20:30:00
>
> CSS Angle TLM 0.976787
>
> CSS Sun-Pointing Angle 1.953574
>
>   25 Oct 23 at 01:00:00
>
> *Pre-Burn *
>
> Thruster 1 13248 17 Oct 23 at 20:30:00
>
> Thruster 2 12880
>
> Thruster 3 16912
>
> Thruster 4 17280
>
> *Post-Burn *
>
> Thruster 1 13440 25 Oct 23 at 01:00:00
>
> Thruster 2 13072
>
> Thruster 3 17328
>
> Thruster 4 17696
>
> *Number of Pulses *
>
> Thruster 1 192
>
> Thruster 2 192
>
> Thruster 3 416
>
> Thruster 4 416
>
> *Thruster Pairs *
>
> Thruster 1 & 2 384
>
> Thruster 3 & 4 832
>
> Timothy E.Perry
>
> CRS IBEX OCO-2
>
> Mission Operations
>
> timothy.perry at ngc.com <mailto:timothy.perry at ngc.com>
>
> Office (703) 406-5976
>
> Cell (301) 606-1430
>

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