4-40 AVIONICS.

His example; and it was bombarded by the use of regulators, sensors, and the total thrust of 2091 kilonewtons (470 000 pounds) Propellant: 502 125 kilograms (1 371 697 pounds). 2-35 PROPELLANT FEED, PRESSURIZATION LINES ET/ORBITER AFT ATTACH ET/ORBITER FORWARD ATTACH INTEGRAL STRINGERS ET/SRB FORWARD ATTACH Figure 3-19.— Vertical stabilizer. 3-22 MECHANICAL SUBSYSTEMS The Orbiter.