Example Essays Home
FAQ
Acceptable Use Policy
Tech Support
LOG IN!
Click HERE for Instant Access
 
This is a free preview of the paper.
Join Now
Log In
  

KC-135 Stratotanker

Historical Information The first KC-135A entered the U.S. Air Force fleet in 1957; the last was delivered in 1965. About 550 of the 732 tankers built, all by Boeing at its Seattle facilities, remain in service. In addition, Boeing built 88 similar aircraft for other Air Force uses, such as flying command posts, pure transports, electronic reconnaissance and photo mapping. The last of these special-purpose aircraft was delivered in late 1966. Tanker Characteristics The KC-135 is equipped with a flying boom for fuel transfer; a special drogue can be attached to the boom on the ground so it can refuel probe-equipped aircraft. An operator stationed in the rear of the airplane controls the boom. A deck above the fuselage-mounted tanks can hold passengers and cargo.In the past 20 years, refueling requirements of the armed services have more than doubled, making the KC-135 an extremely valuable national resource. Modification programs at Boeing have contributed to the life and performance of the airplane. Those efforts include wing re-skinning and the KC-135R and KC-135E re-engining programs. KC-135 Reskinning Program A major program to replace lower wing surfaces on the aircraft was completed in 1988, with a total


of 746 C/KC-135 aircraft — most of them tankers — modified over a 13-year period. The work involved replacing about 1,500 square feet of aluminum of the underside of the wings, which carry most of the wing load in flight, with an improved aluminum alloy. The original wing surface consisted of a type of aluminum more susceptible to fatigue. Skin panels were milled, machined and contoured at Boeing. The wing then went into a rivet assembly jig where stiffeners and skins were joined. The bottom section of the old wing was cut away and replaced by the new sections. In addition to the skin panels, engine strut fitting also were replaced. Each unit required a total of 564 parts, 32,200 steel fasteners and 19,500 aluminum rivets. CFM Re-engine Program Because the KC-135A's original engines are of 1950s technology, they don't meet modern standards for increased fuel efficiency, reduced pollution and noise levels. By installing new CFM56 engines, performance is enhanced and fuel off-load capability if dramatically improved. In fact, the modernization is so successful, two re-engined KC-135R can do the work of three KC-135As. This improvement is a result of the KC-135's lower fuel consumption and increase

Some topics in this essay:
Air Force, Reskinning Program, National Guard, Re-engining CFM56, Characteristics KC-135, KC-135R KC-135As, Program KC-135A's, Air Force's, Boeing Seattle, air force, United KC-135R, cfm56 engines, kc-135e re-engining, square miles, noise levels, skin panels,

Join now to see the rest of the essay!
Approximate Word count = 812
Approximate Pages = 3 (250 words per page double spaced)


  

Join Now
(Credit Card)
Join Now
(Online Check)
Join Now
(Phone 1-900)



CUSTOMER SERVICES




Acceptance Essays
Arts
Custom Essays
English
Foreign
History
Miscellaneous
Movies
Music
Novels
People
Politics
Religion
Science
Sports
Technology
Book Notes

 

 


All papers are for research and references purposes only!
Copyright © 2002-2009 ExampleEssays.com DMCA
Saved Papers