[Isocops] IBEX Goat Herder for 15 June 20
Wesley, Sheral R [US] (IS)
Sheral.Wesley at ngc.com
Fri Jun 19 17:03:43 EDT 2020
All,
The perigee contacts for Orbit# 490 were nominal for command and telemetry.
The Master_Timer command was executed, and the inertial maneuver successful.
Please the following:
1. Set_downlink (320k)
2. SSR_Dump (reset pointers)
3. CAR# 2002 Upload Orbit# 493 BUS/INST ATS
IBEX_2020_185_o0493a_BUS_v001.scr (173-223)
IBEX_2020_185_o0493a_INST_v001.scr (270-315)
4. CAR# 1099 Orbit# 491 Hi Background Test
Mode_HVENG
Mode_HVSTANDBY
Sweep Table Upload_160922 (table_hi_023456_background, quit)
Mode_HVENG
Mode_HVSCI
-0.32969400 ActNor.EstInrToBdy[0]
-0.44081200 ActNor.EstInrToBdy[1]
-0.73710400 ActNor.EstInrToBdy[2]
0.39200000 ActNor.EstInrToBdy[3]
1276302726 ActNor.EstTime
J2000 Spin Axis
ECI X 0.140441
ECI Y 0.908329
ECI Z 0.393973
Precession Maneuver
MPS Diff 0.686 deg
*MPS Diff should be < 1.5
Right Ascension - RA 81.211 deg
Declination - DEC 23.202 deg
IBEX Spin Axis vs. Sun Vector
IBEX Sun Angle -3.429 deg
MPS Cmd Vector X 0.132901000
MPS Cmd Vector Y 0.912901000
MPS Cmd Vector Z 0.385938000
CSS Angle TLM 0.744936
CSS Sun-Pointing Angle 1.489872
10 June 20 @15:00
CSS Angle TLM 0.683569
CSS Sun-Pointing Angle 1.367138
15 June 20 @ 23:30
Pre-Burn
Thruster 1 10800 10 June 20 @15:00
Thruster 2 10496
Thruster 3 13488
Thruster 4 13792
Post-Burn
Thruster 1 11072 15 June 20 @ 23:30
Thruster 2 10768
Thruster 3 13776
Thruster 4 14080
Number of Pulses
Thruster 1 272
Thruster 2 272
Thruster 3 288
Thruster 4 288
Thruster Pairs
Thruster 1 & 2 544
Thruster 3 & 4 576
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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