[Isocops] IBEX Goat Herder for 20-21 April 2021
Wesley, Sheral R [US] (SP)
Sheral.Wesley at ngc.com
Thu Apr 22 01:58:46 EDT 2021
All,
The perigee contacts were nominal for CMD & TLM. The inertial maneuver and master_reset command executed successfully.
The following objectives were accomplished:
1. CAR #1162 SSR_Dump Orbit# o523
2. CAR #1163 Upload Orbit# 526 ATS
a. Bus: IBEX_2021_120_o0526a_BUS_v001 (551-596)
b. Inst; IBEX_2021_120_o0526a_INST_v001 (597-642)
3. SSR_Dump (NEW)
4. Dump_Backorbit
Inertial Maneuver Results:
Q1 0.46967000 ActNor.EstInrToBdy[0]
Q2 0.42779100 ActNor.EstInrToBdy[1]
Q3 0.74282000 ActNor.EstInrToBdy[2]
Q4 0.21124500 ActNor.EstInrToBdy[3]
GPS sec 1303068547 ActNor.EstTime
UTC time 04/21/2021 19:28:53 output
MPS Cmd Vector X 0.874234000
MPS Cmd Vector Y 0.448948000
MPS Cmd Vector Z 0.184826000
CSS Angle TLM 0.678108
CSS Sun-Pointing Angle 1.356216
16 Apr 21 @ 13:00:00
CSS Angle TLM 0.45584
CSS Sun-Pointing Angle 0.91168
21 Apr 21 @ 19:30:00
Pre-Burn
Thruster 1 5504 16 Apr 21 @ 13:00:00
Thruster 2 5344
Thruster 3 7200
Thruster 4 7360
Post-Burn
Thruster 1 5792 21 Apr 21 @ 19:30:00
Thruster 2 5632
Thruster 3 7504
Thruster 4 7664
Number of Pulses
Thruster 1 288
Thruster 2 288
Thruster 3 304
Thruster 4 304
Thruster Pairs
Thruster 1 & 2 576
Thruster 3 & 4 608
Sheral Wesley | 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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