All,

  The perigee passes were nominal for CMD and TLM. The Inertial maneuver was successful.  

We completed the following:

SSR Dump -> Dump New

CAR #1040 Dump Orbit #448 Missing blocks

CAR #1041 ATS upload – IBEX_2019_170_o0451a_v001

Reset Master Timer

Set Spacecraft Clock

 

Result from the Inertial maneuver:

Q1 -0.34657700 ActNor.EstInrToBdy[0]

Q2 -0.43152700 ActNor.EstInrToBdy[1]

Q3 -0.76186200 ActNor.EstInrToBdy[2]

Q4 0.33650500 ActNor.EstInrToBdy[3]

GPS sec 1244220803.000 ActNor.EstTime

MPS Diff 0.707 deg

MPS Cmd Vector X 0.230781000

MPS Cmd Vector Y 0.896300000

MPS Cmd Vector Z 0.378665000

CSS Angle TLM 0.668811

CSS Sun-Pointing Angle 1.337622

  5  June 19 @ 13:00

CSS Angle TLM 0.859118

CSS Sun-Pointing Angle 1.718236

  10 June 19 @ 02:00

Pre-Burn   

Thruster 1 12368 5  June 19 @ 13:00

Thruster 2 12048

Thruster 3 14768

Thruster 4 15088

Post-Burn  

Thruster 1 12640 10 June 19 @ 02:00

Thruster 2 12320

Thruster 3 15072

Thruster 4 15392

Number of Pulses  

Thruster 1 272

Thruster 2 272

Thruster 3 304

Thruster 4 304

Thruster Pairs 

Thruster 1 & 2 544

Thruster 3 & 4 608

 

 

 

Timothy E. Perry

Mission Operations

CRS, IBEX, OCO-2 & TESS

RAPTOR Test Team

timothy.perry@ngc.com

Office (703) 406-5976

Cell (301) 606-1430

 

 



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