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Boeing NC-135

Military Aircraft

The Boeing NC-135 and NKC-135 are special versions of the Boeing C-135 Stratolifter and KC-135 Stratotanker, modified to operate on several different programmes. Sandia National Laboratories configured three NC-135 aircraft as flying laboratories for the Test Readiness Program, begun in 1963 after the Limited Test Ban Treaty, to support atmospheric nuclear testing should it resume; they were based at Kirtland Air Force Base and served until 1976. Their science teams also used them to study solar eclipses, cosmic rays and ionospheric magnetic fields, flying the first eclipse mission from Pago Pago in 1965. Other conversions include the two Big Crow electronic warfare test-beds, one of which served as the target when the YAL-1 airborne laser fired in flight in March 2007, and the NKC-135A that carried a carbon dioxide laser in the Airborne Laser Lab from 1975 to 1984.

Facts
Year
1963 1
Engine Class
Jet 1
Top Speed (km/h)
980 1
Mass (kg)
55,792 1
Maximum Mass (kg)
122,470 1
Engine
Pratt & Whitney J57-P-43WB turbojet (NKC-135A) 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes

An aircraft, so it exemplifies the aviation mode.

Source Boeing NC-135 (Wikipedia)

Of Make

Boeing built this type.

Source Boeing NC-135 (Wikipedia)
In the Other Atlases

Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Boeing NC-135 (Wikipedia)Lead, manufacturer
Quote, Lead, manufacturer
The Boeing NC-135 and NKC-135 are special versions of the Boeing C-135 Stratolifter

Originated In

Also in Geography Atlas: where this subject originated.

Source Boeing NC-135 (Wikipedia)Lead, country of origin
Quote, Lead, country of origin
United States Air Force
Sources
1. Boeing NC-135 (Wikipedia)
  • Readiness Program, conversion start
    Work was initiated in 1963 and the aircraft remained in service until 1976
  • Specifications (NKC-135A), engine
    Powerplant: 4 × Pratt & Whitney J57-P-43WB turbojet engines, 13,750 lbf (61.2 kN) thrust each with water-injection for take-off
  • Specifications (NKC-135A), empty mass
    Empty weight: 123,000 lb (55,792 kg) operating weight empty
  • Specifications (NKC-135A), maximum takeoff
    Max takeoff weight: 270,000 lb (122,470 kg)
  • Specifications (NKC-135A), speed
    Maximum speed: 610 mph (980 km/h, 530 kn) at high altitude
  • Lead
    special versions of the Boeing C-135 Stratolifter and Boeing KC-135 Stratotanker
  • Lead, manufacturer
    The Boeing NC-135 and NKC-135 are special versions of the Boeing C-135 Stratolifter
  • Lead, country of origin
    United States Air Force
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