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Boeing Military Boeing KC-135 Stratotanker

Role Aerial refueling tanker and transport aircraft
]National origin United States
Manufacturer Boeing
First flight 31 August 1956 Introduction June 1957
Status In service
Primary users United States Air Force French Air and Space Force Turkish Air Force Republic of Singapore Air Force
Produced 1955–1965
Number built 803 Developed from Boeing 367-80
Variants Boeing C-135 Stratolifter Boeing EC-135 Boeing NC-135 Boeing OC-135B Open Skies Boeing RC-135 Boeing WC-135 Constant Phoenix

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History Boeing Military
Boeing KC-135 Stratotanker 



The Boeing KC-135 Stratotanker is an American military aerial refueling tanker aircraft that was developed from the Boeing 367-80 prototype, alongside the Boeing 707 airliner. It has a narrower fuselage and is shorter than the 707. Boeing gave the aircraft the internal designation of Model 717. The KC-135 was the United States Air Force's first jet-powered refueling tanker and replaced the KC-97 Stratofreighter. The KC-135 was initially tasked with refueling strategic bombers, but it was used extensively in the Vietnam War and later conflicts such as Operation Desert Storm to extend the range and endurance of US tactical fighters and bombers.

The KC-135R has four turbofan engines, mounted under 35-degree swept wings, which power it to takeoffs at gross weights up to 322,500 pounds (146,300 kg). Nearly all internal fuel can be pumped through the tanker's flying boom, the KC-135's primary fuel transfer method. A boom operator stationed in the rear of the aircraft controls the boom while lying prone, viewing through a window at the bottom of the tail. Both the flying boom and operator's station are similar to those of the previous KC-97. A special shuttlecock-shaped drogue, attached to and trailing behind the flying boom, may be used to refuel aircraft fitted with probes. This apparatus is significantly more unforgiving of pilot error in the receiving aircraft than conventional trailing hose arrangements; an aircraft so fitted is also incapable of refueling by the normal flying boom method until the attachment is removed. A cargo deck above the refueling system can hold a mixed load of passengers and cargo. Depending on fuel storage configuration, the KC-135 can carry up to 83,000 pounds (38,000 kg) of cargo.

The KC-135 was initially purchased to support bombers of the Strategic Air Command, but by the late 1960s, in the Southeast Asia theater, the KC-135 Stratotanker's ability as a force multiplier came to the fore. Midair refueling of F-105 and F-4 fighter-bombers as well as B-52 bombers brought far-flung bombing targets within reach, and allowed fighter missions to spend hours at the front, rather than a few minutes, which was usual due to their limited fuel reserves and high fuel consumption. KC-135 crews refueled both Air Force and Navy / Marine Corps aircraft; though they would have to change to probe and drogue adapters depending upon the mission, the Navy and Marine Corps not having fitted their aircraft with flying boom receptacles since the USAF boom system was impractical for aircraft carrier operations. Crews also helped to bring in damaged aircraft which could sometimes fly while being fed by fuel to a landing site or to ditch over the water (specifically those with punctured fuel tanks). KC-135s continued their tactical support role in later conflicts such as Operation Desert Storm and current aerial strategy. 

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Boeing BCA Militaryl

Boeing Military Airplanes
Boeing KC-135 Stratotanker

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General characteristics

  • Crew: 3 (pilot, co-pilot and boom operator; some KC-135 missions require the addition of a navigator.)
  • Capacity: up to 80 passengers / 83,000 lb (38,000 kg) or 6 463L pallets
  • Length: 136 ft 3 in (41.53 m)
  • Wingspan: 130 ft 10 in (39.88 m)
  • Height: 41 ft 8 in (12.70 m)
  • Wing area: 2,433 sq ft (226.0 m2)
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Powerplant

  • Empty weight:  (44,630 kg)
  • Operating empty weight:  (56,245 kg)
  • Gross weight:  (134,717 kg)
  • Max takeoff weight:  (146,284 kg)
  • Fuel capacity: (90,718 kg)
  • Powerplant: 4 × CFM International F108-CF-100 turbofan engines, 21,600 lbf (96.2 kN) thrust each
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Specifications

  • Maximum speed:, 933 km/h)
  • Maximum speed: Mach 0.9
  • Cruise speed: , 852.8 km/h)
  • Range: (2,414.1 km)  (68,039 kg) 
  • Ferry range:   17,727 km)
  • Service ceiling:  (15,000 m)
  • Rate of climb: 4,900 ft/min (25 m/s)
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Boeing KC-135 Stratotanker

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Boeing KC-135 Stratotanker

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Youtube Link

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