Guys,

The perigee tracking contact for Orbit# 319 was nominal for command/telemetry and the sun maneuver successful

CSS Telemetry data was collected and will be used to set the CEU default spin rate on 14 Mar 16 @1500 UTC

1.reset_master_timer.scr

2. ops_set_sc_time.scr

3. @FTG_DumpBackorbit(from start,0,0,0,0)

4. CAR# 805 CSS telemetry/CEU Default spin rate

a. css_telemetry_v002.scr

5. VC0= 1909 with 1 error

6. VC1= 1314 with 0 errors

CSS Angle TLM	2.68999	13 Mar 16 @1000
CSS Sun-Pointing Angle	5.37998
CSS Sun-Pointing Angle	5.37998
CSS Angle TLM	1.083	14 Mar 16 @0730
CSS Sun-Pointing Angle	2.166
CSS Sun-Pointing Angle	2.166
Pre-Burn
Thruster 1	8416	13 Mar 16 @1000
Thruster 2	8192
Thruster 3	10208
Thruster 4	10432
Post-Burn
Thruster 1	8640	14 Mar 16 @0730
Thruster 2	8384
Thruster 3	10528
Thruster 4	10784
Number of Pulses
Thruster 1	224
Thruster 2	192
Thruster 3	320
Thruster 4	352
Thruster Pairs
Thruster 1 & 2	416
Thruster 3 & 4	672

Sheral R. Wesley

IBEX Mission OPS

CRS/CYGNUS Mission Planning

Bldg. 2 Room 1337

Office (703) 406-5641

Cell (202) 236-0802

cid:image001.jpg@01D04F6C.5A1C97F0

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