,

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

The following was accomplished:

SSR Dump -> Dump New

Set the SSR read and write pointers to 70000

Reset master timer

Dumped FC back orbit data

Reset FDC Totals

CAR # 1026 – ATS upload Orbit #441

   IBEX _2019_078_o0441_v001 88 Cmds

CAR # 1027 – Dump Orbit 439 Missing Blocks

   Dumped 30 Blocks no errors

CAR # 1028 – ATS upload Orbit # 441 Contact

   IBEX _2019_078_o0441a_0400_Contact_V001 5 Cmds

 

 

Results from the Inertial maneuver:

Q1 0.14553600 ActNor.EstInrToBdy[0]

Q2 0.71486500 ActNor.EstInrToBdy[1]

Q3 0.02916890 ActNor.EstInrToBdy[2]

Q4 0.68332800 ActNor.EstInrToBdy[3]

GPS sec 1236232896.000 ActNor.EstTime

MPS Diff 0.822 deg

MPS Cmd Vector X 0.986167000

MPS Cmd Vector Y -0.147736000

MPS Cmd Vector Z -0.075153000

CSS Angle TLM 0.206534

CSS Sun-Pointing Angle 0.413068

  08 Mar 19 @20:00

CSS Angle TLM 1.03929

CSS Sun-Pointing Angle 2.07858

  10 Mar 19 @06:00

Pre-Burn   

Thruster 1 7296 08 Mar 19 @20:00

Thruster 2 7120

Thruster 3 8720

Thruster 4 8896

Post-Burn  

Thruster 1 7568 10 Mar 19 @06:00

Thruster 2 7392

Thruster 3 9008

Thruster 4 9184

Number of Pulses  

Thruster 1 272

Thruster 2 272

Thruster 3 288

Thruster 4 288

Thruster Pairs 

 

 

Timothy E.Perry

CRS IBEX OCO-2

Mission Operations

tim.perry@orbitalatk.com

Office (703) 406-5976

Cell (301) 606-1430

cid:image001.jpg@01D04F4E.6B1BECE0

 

 
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