[Isocops] IBEX Orbit# 242 Apogee Contact

[Ibex Mission Operations]

The Apogee Contact for Orbit# 242 was nominal for command/telemetry and the
inertial maneuver successful.

*RAZOR# 577* was issued for the following reason:
The IBEX CMD1 Workstation loacked up during a contact with USN/HAW01 @2018
UTC. The telemetry/command sockets from USN were dropped by USN prior to
rebooting the work station to avoind hanging the sockets during the
rebooting sequence.
The workstation was back online @ 2028 UTC

The following objectives were accomplished

1. CAR# 676 Upload Orbit# 243 ATS
IBEX_2014_103_o0243a_v001.scr (487-590)


*Date*                                     *Jday*     *Time*
*Station*
*Razor#*       *USNPR#*       *PASS/FAIL*

   *Thursday, April 10, 2014*         100       2000       USHI01
577                                     Pass

*Controller*     *CAR1*      *CAR2*    *CAR3*    *Radius Earth*    *S-Band
Rate*      *Station PWR*

   SWesley        676                                    41 desc
2ksps               200 watts

  *EBNO Values*                            *EBNO Values 3*
*AGC Strength*

       @2000=13.06-15.32
@2000=-121.17db(2k)

  *EBNO Values 2*
*AGC Strength 2*

      @2017=0db (40ksps)

  *VC 0*          *VC 0 Seq Err*           *VC 1*     *VC 1 Seq Err*       *VC
2*       *VC 2 Seq Err *

    158                     3                       0
0
0                   0

  *VC 2 Write Pointer Start*      46380             *VC 2 Write
Pointer End*
46456

  *VC 2 Read Pointer Start*        28958             *VC 2 Read
Pointer End*
28950

  Orbit# 242 Apogee Contact

CAR# 676 Upload Orbit# 243 ATS  1.IBEX_2014_103_o0243a_v001.scr (487-590)

@FMI_SetDownlink(40k)

@FMI_SetDownlink (2k)

Reboot CMD1 Workstation



  IBEX Orbit# 243 APOGEE Target Vectors 10 Apr 14

  J2000  Spin Axis

  ECI X    0.960854

  ECI Y    0.253438

  ECI Z    0.111930



  Precession Maneuver

  MPS Diff             0.834      deg

  * MPS Diff should be < 1.5*



  0.53806600        ActNor.EstInrToBdy[0]

  0.39309000        ActNor.EstInrToBdy[1]

  0.69434500        ActNor.EstInrToBdy[2]

  0.27175300         ActNor.EstInrToBdy[3]

  1081200000.000                ActNor.EstTime



  Right Ascension - RA          14.776    deg

  Declination - DEC                6.427      deg



  IBEX Spin Axis vs. Sun Vector

  IBEX Sun Angle  -4.845    deg



  IBEX MPS Generated Target Vectors

  MPS Cmd Vector X             0.958507000

  MPS Cmd Vector Y             0.265403000

  MPS Cmd Vector Z             0.104042000



    CSS Angle TLM 0.801619  CSS Sun-Pointing Angle 1.603238  4 Apr 14 @1000 CSS
Angle TLM 1.93097  CSS Sun-Pointing Angle 3.86194  10 Apr 14 @2000
*Pre-Burn*     Thruster 1 17824 4 Apr 14 @1000 Thruster 2 17408  Thruster 3
19488  Thruster 4 19904  *Post-Burn*   Thruster 1 18128 10 Apr 14
@2000 Thruster
2 17680  Thruster 3 19776  Thruster 4 20224  *Number of Pulses*    Thruster
1 304  Thruster 2 272  Thruster 3 288  Thruster 4 320  *Thruster
Pairs*   Thruster
1 & 2 576  Thruster 3 & 4 608







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