All,

   The perigee passes were nominal. APL reported successful SSR dump.

The Inertial Maneuver was nominal.

The following was completed during the SSC/Haw01 support:

CAR # 861 – Change Star Sensor TLM rate

CAR # 860 ATS upload

    IBEX_2016_183_o0333a_v002 108 cmds

Reset Master Timer

Set S/C clock

 

Result from the Inertial maneuver:

Q1 -0.16154900 ActNor.EstInrToBdy[0]

Q2 -0.52618200 ActNor.EstInrToBdy[1]

Q3 -0.74982200 ActNor.EstInrToBdy[2]

Q4 0.36715200 ActNor.EstInrToBdy[3]

GPS sec 1151550000.000 ActNor.EstTime

MPS Cmd Vector X -0.152111000

MPS Cmd Vector Y 0.910640000

MPS Cmd Vector Z 0.384183000

MPS Diff 0.749

28 June 16 @1400

CSS Angle TLM 2.4504

CSS Sun-Pointing Angle 4.9008

03 June 16 @0200

CSS Angle TLM 2.28662

CSS Sun-Pointing Angle 4.57324

  

Pre-Burn    28 June 16 @1400

Thruster 1 14016

Thruster 2 13552

Thruster 3 18144

Thruster 4 18608 

Post-Burn  03 June 16 @0200

Thruster 1 14288

Thruster 2 13824

Thruster 3 18432

Thruster 4 18896 

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

 

All have a Happy 4th  and Go JUNO!!!!!!

 

Timothy E.Perry

CRS, IBEX & OCO-2

Mission Operations

tim.perry@orbitalatk.com

Office (703) 406-5976

Cell (301) 606-1430

Corp Cell (571)-447-8977

cid:image001.jpg@01D04F4E.6B1BECE0

 


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