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Boeing C-135 Stratolifter

Military Aircraft

The Boeing C-135 Stratolifter is a transport aircraft developed from the Boeing KC-135 Stratotanker and the basis of a number of variants performing different roles; the first was built in August 1956 and the C-135 and its variants have been a fixture of the United States Air Force ever since. In the early 1960s the Military Air Transport Service flew almost entirely propeller-driven aircraft such as the Douglas C-124 Globemaster II and the turboprop C-133 Cargomaster, which were becoming obsolescent, and in May 1960 Congress approved the purchase of 50 C-135s, chosen partly for the low development cost of a straightforward KC-135 derivative. Only 15 C-135As were produced, plus three converted on the assembly line, and 30 more were delivered as C-135Bs with Pratt & Whitney TF33 turbofans. It was an interim measure, with a load floor about 10 feet off the ground, a single side cargo door and no aerial refuelling receptacle.

Facts
Year
1956 1
Engine Class
Jet 1
Top Speed (km/h)
933 1
Mass (kg)
44,663 1
Maximum Mass (kg)
146,000 1
Engine
Pratt & Whitney TF33-PW-102 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes

An aircraft, so it exemplifies the aviation mode.

Source Boeing C-135 Stratolifter (Wikipedia)

Of Make

Boeing built this type.

Source Boeing C-135 Stratolifter (Wikipedia)
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Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Boeing C-135 Stratolifter (Wikipedia)Lead, manufacturer
Quote, Lead, manufacturer
The Boeing C-135 Stratolifter is a transport aircraft developed from the Boeing KC-135 Stratotanker

Originated In

Also in Geography Atlas: where this subject originated.

Source Boeing C-135 Stratolifter (Wikipedia)Lead, country of origin
Quote, Lead, country of origin
have been a fixture of the United States Air Force
Sources
1. Boeing C-135 Stratolifter (Wikipedia)
  • Lead, first build
    Since the first one was built in August 1956
  • Specifications (C-135), engine name
    Powerplant: 4 × 4 Pratt & Whitney TF-33-PW-102 low-bypass turbofan engines , 18,000 lbf (80 kN) thrust each
  • Specifications (C-135), empty mass
    Empty weight: 98,466 lb (44,663 kg)
  • Specifications (C-135), maximum takeoff
    Max takeoff weight: 322,500 lb (146,000 kg)
  • Specifications (C-135), speed
    Maximum speed: 580 mph (933 km/h, 500 kn)
  • Lead
    is a transport aircraft developed from the Boeing KC-135 Stratotanker
  • Lead, manufacturer
    The Boeing C-135 Stratolifter is a transport aircraft developed from the Boeing KC-135 Stratotanker
  • Lead, country of origin
    have been a fixture of the United States Air Force
  • In Group: Military Transport Aircraft, Lead, role
    is a transport aircraft developed from the Boeing KC-135 Stratotanker
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