All,

   The Apogee contacts were nominal for CMD and TLM. The Sun Maneuver was successful. The SSR was dumped and the orbit #495 bus ats was uplinked. The Master Timer Reset command executed nominally. We do have a problem with receiving the VC files post pass. SSC has been notified and they are looking into why they are not being sent.

 

Tasks Accomplished:

SSR Dump -> Dump New

CAR 1100 ATS upload – IBEX_2020_204_O0495A_BUS_V001  48 CMDS

 

 

Results from the Sun Maneuver

CSS Angle TLM 1.63996

CSS Sun-Pointing Angle 3.27992

  29 June 20 @ 12:00

CSS Angle TLM 1.50024

CSS Sun-Pointing Angle 3.00048

  29 June 20 @ 12:00

Pre-Burn   

Thruster 1 11904 29 June 20 @ 12:00

Thruster 2 11568

Thruster 3 14672

Thruster 4 15008

Post-Burn  

Thruster 1 12176 29 June 20 @ 12:00

Thruster 2 11840

Thruster 3 15216

Thruster 4 15552

Number of Pulses  

Thruster 1 272

Thruster 2 272

Thruster 3 544

Thruster 4 544

Thruster Pairs 

Thruster 1 & 2 544

Thruster 3 & 4 1088

 

 

 

 

Timothy E. Perry

Mission Operations

CRS, IBEX, OCO-2

timothy.perry@ngc.com

Office (703) 406-5976

Cell (301) 606-1430