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(Note that A / AUTO / NORM holds orbiter attitude: use UNIV PTG to track -X body vector at center of Earth - orbiter & SPAS are both in LVLH)

4. At 200'-300', [[two hundred to three hundred feet]] 60 to B/ for a smaller pulse size & LO Z to minimize plume impingement => Note that LO Z uses ~9X [[about nine times]] more fuel than norm Z. 

5. Close-in station-keeping at ~100' [[about one hundred feet]] (maybe closer)

* Specific procedures still in work (to minimize fuel, etc)

* Fuel required.... ~2000# [[about two thousand pounds]] (roughly) per 1000' [[one thousand feet]] approach

* Time required - 30-40 [[thirty to forty]] minutes (roughly)