gimbel's in the their start positions. at t minus two minutes and 55 seconds, external tank liquid pressure began. it t minus two minutes 50 seconds, retraction of the gaseous oxygen venter began. crown launcher -- sequence verified its full retraction at t -37 seconds. water wasression started at t -16 seconds. at t minus eight seconds, hydrogen igniters were turned on to burn off any free hydrogen. before launch, challenger's liquid fueled main engines were ignited in sequence and run up to full thrust. thrust from the main engines spec.he shuttle when it returned to vertical the solid rocket boosters ignited. at t zero, the holdout bolts were explosively released. after the initial prerelease twang ocean, structural force is dissipated at a rate of three cycles per second. >> it has cleared the tower. initiated ater was 7.724 seconds. the maneuver was completed at 21.124 seconds. >> normal throttle for most of the flight, 104%. the main engines were throttled after 65% for about 16 seconds in order to alleviate maximum