[Isocops] IBEX Orbit# 159 Apogee Contact
Ibex Mission Operations
ibexops at gmail.com
Fri Mar 16 14:57:11 EDT 2012
Guys,
The Apogee contact for Orbit# 159 was nominal for command/telemetry.
The Sun Maneuver was successful.
The staticZrate will be set on the next contact when we are >90% valid.
1. StaPctValid=59%
2. StaticZRate rpm=4.16641
3. SpinRate (ST)=4.17041
VC0=396 with 4 errors
VC1=1453 with 29 errors
CSS Angle TLM 1.68109 CSS Sun-Pointing Angle 3.36218 3/11/2012 21:09 CSS
Angle TLM 1.1896 CSS Sun-Pointing Angle 2.3792 3/16/2012 18:36 *Pre-Burn
* 3/11/2012 21:09 Thruster 1 1680 Thruster 2 1632 Thruster 3 1840 Thruster
4 1888 *Post-Burn* ** 3/16/2012 18:36 Thruster 1 2032 Thruster 2
1984 Thruster
3 2240 Thruster 4 2288 *Number of Pulses* ** ** Thruster 1 352 Thruster 2
352 Thruster 3 400 Thruster 4 400 *Thruster Pairs* ** ** Thruster 1 & 2
704 Thruster 3 & 4 800
--
Sheral R. Wesley
SPVR., Satellite Operations
IBEX Mission OPS
(304) 279-6678
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