[Isocops] IBEX Orbit# 215 SSR_Dump Contact

[Ibex Mission Operations]

Guys,
    The SSR_Dump contact for Orbit# 215 was nominal for command/telemetry
and the inertial maneuver successful.
The following objectives were accomplished:
1. reset_master_timer.scr
2. SSR_Dump.scr (new)
3. CAR# 634 Upload Orbit# 217 ATS
IBEX_2013_231_o0217a_v001.scr (671-770)


Precession Maneuver

  MPS Diff             0.828      deg

  *MPS Diff should be < 1.5*



  IBEX Spin Zxis (+Z S/C)

  Right Ascension - RA          280.740 deg

  Declination - DEC                -22.918  deg



  IBEX Spin Axis vs. Sun Vector

  IBEX Sun Angle  -1.753     deg



  0.82854500        ActNor.EstInrToBdy[0]

  0.09065390        ActNor.EstInrToBdy[1]

  0.04330860        ActNor.EstInrToBdy[2]

  0.55083600        ActNor.EstInrToBdy[3]
  1041110000.000 ActNor.EstTime


IBEX Orbit# 191 APOGEE Target Vectors  1 Jan 13

  J2000  Spin Axis

  ECI X    0.171637

  ECI Y    -0.904932

  ECI Z    -0.389409

Orbit# 191 MPS Generated APOGEE Target Vectors

  MPS Cmd Vector X             0.178145000

  MPS Cmd Vector Y             -0.898709000

  MPS Cmd Vector Z             -0.400733000


    CSS Angle TLM 2.45232  CSS Sun-Pointing Angle 4.90464  7 Aug 13 @1236 CSS
Angle TLM 0.856837  CSS Sun-Pointing Angle 1.713674  10 Aug 13 @1602 *
Pre-Burn*     Thruster 1 1888 7 Aug 13 @1236 Thruster 2 1856  Thruster 3
1968  Thruster 4 2000  *Post-Burn* ** ** Thruster 1 2160 10 Aug 13
@1602 Thruster
2 2128  Thruster 3 2304  Thruster 4 2336  *Number of Pulses*    Thruster 1
272  Thruster 2 272  Thruster 3 336  Thruster 4 336  *Thruster Pairs*
** ** Thruster
1 & 2 544  Thruster 3 & 4 672



-- 
Sheral R. Wesley
SPVR., Satellite Operations
IBEX Mission OPS
(304) 279-6678
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