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   Generates the data needed for an SPM maneuver in TrnsfOrb.m
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   Form:
   x = SPMDataT( tID, pulsewidth, rAF, decF )
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   Inputs
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   tID           (1,n) Ids of thruster to be used
   pulsewidth    (1,1) Pulsewidth
   rAF           (1,1) Final right ascension
   decF          (1,1) Final declination

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   Outputs
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   x             (1,4+n) Formatted data

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