All,
The perigee contacts for Orbit# 530 were successful for command/telemetry and the inertial maneuver.
The following objectives were accomplished:
1.
Reset_master_timer
2.
SSR_Dump (new)
3.
CAR# 1175 Upload Orbit# 532 ATS (IBEX_2021_175_o0532a_v001 (39-134)
4.
CAR# 1152 IBEX Hi Background tests and Lo 2021 Magnetotail Season
a.
mode_hveng
b.
mode hvstandby
c.
Sweep_table_upload_190922 (Table_Hi_023456_Background, quit)
d.
mode_hveng
e.
mode_hvsci
Orbit# 530 Perigee Maneuver
Q1 -0.21493900 ActNor.EstInrToBdy[0]
Q2 0.50458700 ActNor.EstInrToBdy[1]
Q3 0.71008200 ActNor.EstInrToBdy[2]
Q4 0.44156200 ActNor.EstInrToBdy[3]
GPS sec 1307869159 ActNor.EstTime
UTC time 06/16/2021 08:59:05
MPS Cmd Vector X 0.131669000
MPS Cmd Vector Y 0.913039000
MPS Cmd Vector Z 0.386035000
MPS Diff 0.945 deg
*MPS Diff should be < 1.5*
CSS Angle TLM 0.415901
CSS Sun-Pointing Angle 0.831802
11 June 21 @ 11:00:00
CSS Angle TLM 0.54368
CSS Sun-Pointing Angle 1.08736
16 June 21 @ 09:00:00
Pre-Burn
Thruster 1 2784 11 June 21 @ 11:00:00
Thruster 2 2752
Thruster 3 2960
Thruster 4 2992
Post-Burn
Thruster 1 3088 16 June 21 @ 09:00:00
Thruster 2 3024
Thruster 3 3264
Thruster 4 3328
Number of Pulses
Thruster 1 304
Thruster 2 272
Thruster 3 304
Thruster 4 336
Thruster Pairs
Thruster 1 & 2 576
Thruster 3 & 4 640
Timothy E.Perry
CRS IBEX OCO-2
Mission Operations
timothy.perry@ngc.com
Office (703) 406-5976
Cell (301) 606-1430