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KC-135 Stratotanker

KC-135 Stratotanker

Tanker Aircrafts
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Basic Information
Name
KC-135 Stratotanker
Designation
KC-135 Stratotanker
Alternate Designation
C-135 Stratolifter, C-135C Speckled Trout, C-135F, C-135FR, EC-135, EC-135C, EC-135E, KC-135A, KC-135E, KC-135Q, KC-135R, KC-135T, NC-135E Big Crow (test aircraft), NKC-135, NKC-135A, OC-135, RC-135, RC-135S Cobra Ball, RC-135U, RC-135V Rivet Joint, RC-135W, TC-135W, WC-135M
Equipment Type
Tanker Aircrafts
Manufacturer
Boeing
Date of Introduction
1957
Description

The KC-135 Stratotanker is a tanker aircraft designed to provide refueling for US Air Force, US Navy and USMC aircraft, as well as aircraft from allied nations. The first KC-135 tanker was delivered to the Castle US Air Force Base, California, in June 1957 and the last one in 1965. The KC-135 has an aerial boom as primary fuel transfer method. A special shuttlecock-shaped drogue, attached to and trailing behind the flying boom, may be used to refuel aircraft fitted with probes. In addition, the KC-135 can accommodate passengers and cargo (up to 83,000 pounds) in a deck above the refueling system. As of 2006, the US Air Force's inventory includes 417 KC-135Rs and 112 KC-135Es. The number of E models would drop to 63 aircraft by fiscal year 2011. The future of KC-135 fleet remains uncertain due to a corrosion problem that would escalate into maintenance costs growth. The KC-X tanker replacement program envisages that the last Stratotanker should be retired from the fleet by 2040. Boeing is offering its KC-767 tanker aircraft as replacement for aging KC-135 tankers, while Northrop-Grumman/EADS North America are offering the Airbus A330 MRTT. The deals are on hold pending law suit and further US Air Force and governmental studies. Both tankers will be evaluated by the USAF under the KC-X program. The C-135C Speckled Trout was a variant introduced in the mid 1970s as a VIP transport for the US Air Force chief of staff. This aircraft was retired in early February 2006.

Air & Air Defense Specifications
Crew 4
Max Speed 853.2 km/h
Range 2413.0 km
Service Ceiling 15250 m
Wingspan 39.90 m
Overview (Deagel)
Group Tanker Aircrafts
Status Active
Also Known As C-135 Stratolifter, C-135C Speckled Trout, C-135F, C-135FR, EC-135, EC-135C, EC-135E, KC-135A, KC-135E, KC-135Q, KC-135R, KC-135T, NC-135E Big Crow (test aircraft), NKC-135, NKC-135A, OC-135, RC-135, RC-135S Cobra Ball, RC-135U, RC-135V Rivet Joint, RC-135W, TC-135W, WC-135M
Origin United States of America
Contractor Boeing
Initial Operational Capability (IOC) June 1957
Total Production 732
Unitary Cost USD $40 million
Specifications (Deagel)
Crew 4
Number of Engines 4
Passengers 37
Dimensions — Height 12.7 meter
Dimensions — Length 41.5 meter
Dimensions — Wingspan 39.9 meter
Mass — Max Takeoff Thrust 105,200 pound
Mass — Max Takeoff Weight 146 ton
Mass — Payload 37,650 kilogram
Performance — Ceiling 15,250 meter
Performance — Max Range 2,413 kilometer
Speed — Top Speed at High Altitude 237 mps
Gear (Deagel)
Item 1 Jamming Systems: LAIRCM G3
Item 2 Radar Systems: AN/APN-242 (1)
Item 3 Turbofan Engines: CFM56-2 (4)
Item 4 Turbofan Engines: TF33 (4)
Details
Country of Origin United States
Category Aerial Refueling Aircraft
Air > Aerial Refueling Aircraft
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
41.5 m
Width
39.9 m
Height
12.7 m
Weight
146000 kg
Operators (5)
United States
France
United Kingdom
Chile
Singapore
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