RCS systems. After propellant loading.

(25 pounds) Liquid hydrogen: 102618 kilograms (226 237 pounds) Total: 719 112 kilograms (1 371 697 pounds). 2-35 PROPELLANT FEED, PRESSURIZATION LINES ET/ORBITER AFT ATTACH ET/ORBITER FORWARD ATTACH Figure 3-19.— Vertical stabilizer. 3-22 MECHANICAL SUBSYSTEMS The Orbiter landing impact. The shock struts.