QUOTE (jabe @ Oct 6 2007, 10:10 PM)

Efficiency issues using fuel resources sometimes has multiple perigee burns to increase the apogee to the required size..which is why I believe the probe did several orbits around the Earth. (I may be wrongabout why multiple burns though

)
A couple of factors play in. One, ideally the delta-V should be impulsive (i.e. instantaneous, with infinite thrust)
But that means infinite structural loads, and a big engine. With a real engine, the thrusting must be conducted
over a finite time, i.e. a finite orbital arc. If the vehicle is spin-stabilized, and the arc is long, then the
engine suffers a cosine loss in useful thrust at the ends of the arc, and so it can be more efficient to split the
burn up into smaller ones (each with lower losses). There can also be issues of orbit determination or safety
(e.g. that should a burn fail part way through, you arent left in some catastrophic orbit - sometimes splitting
it up can avoid danger zones) but that is less likely here.