[Isocops] IBEX Goat Herder for 27 April 2020
Wesley, Sheral R [US] (IS)
Sheral.Wesley at ngc.com
Mon Apr 27 19:20:12 EDT 2020
All,
The Apogee contact was monitored via NX and was nominal for telemetry. The command link was established for Doppler
Results from the Inertial Maneuver:
0.52369100
ActNor.EstInrToBdy[0]
0.33594400
ActNor.EstInrToBdy[1]
0.78285900
ActNor.EstInrToBdy[2]
0.00452018
ActNor.EstInrToBdy[3]
1272029805
ActNor.EstTime
UTC time
04/27/2020 13:36:31
MPS Cmd Vector X
0.818630000
MPS Cmd Vector Y
0.530873000
MPS Cmd Vector Z
0.219131000
Right Ascension - RA
32.349
deg
Declination - DEC
13.049
deg
IBEX Spin Axis vs. Sun Vector
IBEX Sun Angle
-3.153
deg
Precession Maneuver
MPS Diff 0.716 deg
MPS Diff should be < 1.5
CSS Angle TLM
0.387149
CSS Sun-Pointing Angle
0.774298
23 Apr 20 @ 05:00
CSS Angle TLM
0.53803
CSS Sun-Pointing Angle
1.07606
27 Apr 20 @ 13:00
Pre-Burn
Thruster 1
7968
23 Apr 20 @ 05:00
Thruster 2
7696
Thruster 3
10256
Thruster 4
10528
Post-Burn
Thruster 1
8240
27 Apr 20 @ 13:00
Thruster 2
7968
Thruster 3
10544
Thruster 4
10816
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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