Kc 135 Engineering Schematics

The maximum fuel load of the variant kc 135r is 90 719 kg 200 000 lb.
Kc 135 engineering schematics. The usaf ordered the aircraft into production as the kc 135 aerial refueling aircraft. The boeing kc 135 stratotanker is a four engined air to air tanker and cargo aircraft produced by the us american manufacturer boeing company. Mission the kc 135 stratotanker provides the core aerial refueling capability for the united states air force and has excelled in this role for more than 60 years. The kc 135 was basically powered by pratt whitney j57 p 59w turbojet engines 61 2 kn 13750 lbf.
The us air force still has about 550 kc 135 stratotankers in service active duty 253. The fuel cells are made of nylon fabric less than one sixteenth of an inch thick a cell weighing 80 pounds will hold seven tons of fuel. This unique asset enhances the air force s capability to accomplish its primary mission of. Air force reserve 70 and has made substantial investment in a series of upgrade programs including reskinning of the lower wing surfaces the installation of new cfm56 engines and new avionics systems.
A large number of variants of both basic models have been used in us and foreign. Cross sectional height of 164 inches. Boeing built 732 kc 135 stratotankers for the us air force between 1957 and 1965. Air national guard 222.
The 707 138 and 720 are 20 inches longer the 707 120 is 120 inches longer and the. 1 the kc 135 fuselage is the same length as 367 80 s. Boeing developed a slightly larger version of the aircraft as the boeing 707 airliner which first entered service in 1958.