All,
The perigee contacts were nominal for command, but had intermittent telemetry during the 1st SSR data dump @0200z and had to decrease the telemetry rate to 160k. The 2nd contact
was changed from HAW01 to AK01 @320k and extended in order to redump the SSR data from orbit# 668.
Objectives during the contacts
IBEX_2024_327_o0669a_v001-lgc (573-627)
IBEX_2024_327_o0669a_v001 (628-725)
ssr_dump NBLOCKS (Start 96870 Numblks 95860)
Results from the PERIGEE maneuver
Q1 -0.18792700 ActNor.EstInrToBdy[0]
Q2 -0.79515800 ActNor.EstInrToBdy[1]
Q3 0.53679500 ActNor.EstInrToBdy[2]
Q4 0.21037800 ActNor.EstInrToBdy[3]
GPS sec 1416281509 ActNor.EstTime
UTC time 11/22/2024 03:31:35 output
MPS Diff 0.588 deg
*MPS Diff should be < 1.5
MPS Cmd Vector X -0.53291600
MPS Cmd Vector Y -0.77276500
MPS Cmd Vector Z -0.34472500
CSS Angle TLM 1.873
CSS Sun-Pointing Angle 3.746
17 Nov 24 @21:00:00
CSS Angle TLM 0.502411
CSS Sun-Pointing Angle 1.004822
22 Nov 24 @02:30:00
Pre-Burn
Thruster 1 9312 17 Nov 24 @21:00:00
Thruster 2 9056
Thruster 3 11296
Thruster 4 11552
Post-Burn
Thruster 1 9456 22 Nov 24 @02:30:00
Thruster 2 9200
Thruster 3 11456
Thruster 4 11712
Number of Pulses
Thruster 1 144
Thruster 2 144
Thruster 3 160
Thruster 4 160
Thruster Pairs
Thruster 1 & 2 288
Thruster 3 & 4 320
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