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        Policy UpdatesNewsroomReoptimizationBIOGRAPHIESAF Senior Leaders   B-roll of WC-135 Constant Phoenix. (U.S. Air Force)
                
                
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        Throughout the afternoon, an WC-135W Constant Phoenix aircraft performs touch 'n go landing exercises Feb. 12 at Offutt Air Force Base, Neb. (U.S. Air Force photo/Josh Plueger)Throughout the afternoon, an WC-135W Constant Phoenix aircraft performs touch 'n go landing exercises Feb. 12 at Offutt Air Force Base, Neb. (U.S. Air Force photo/Josh Plueger)
                
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        WC-135 Constant PhoenixThe WC-135 Constant Phoenix sits on the runway at Patrick AFB, Fla., during a visit to the base where its main mission headquarters, the Air Force Technical Applications Center, is located. The specially-configured aircraft is equipped with external flow devices that allow special equipment operators to collect airborne particulates in support of the U.S. Atomic Energy Detection System in the event of a nuclear detonation. (U.S. Air Force photo by Susan A. Romano)
                
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        FILE PHOTO -- The WC-135W Constant Phoenix aircraft collects particulate and gaseous debris from the accessible regions of the atmosphere in support of the Limited Nuclear Test Ban Treaty of 1963. (U.S. Air Force photo)The WC-135W Constant Phoenix aircraft collects particulate and gaseous debris from the accessible regions of the atmosphere in support of the Limited Nuclear Test Ban Treaty of 1963. (U.S. Air Force photo)
                
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 WC-135 Constant Phoenix**Mission**
The WC-135W Constant Phoenix atmospheric collection aircraft supports national level consumers by collecting particulate and gaseous effluents and debris from accessible regions of the atmosphere in support of the Limited Nuclear Test Ban Treaty of 1963.**Features**
The aircraft is a modified C-135B or EC-135C platform. The Constant Phoenix's modifications are primarily related to its on-board atmospheric collection suite, which allows the mission crew to detect radioactive "clouds" in real time. The aircraft is equipped with external flow-through devices to collect particulates on filter paper and a compressor system for whole air samples collected in holding spheres.
The cockpit crew is from the 45th Reconnaissance Squadron at Offutt Air Force Base, Neb., and special equipment operators are assigned to Det. 1, Air Force Technical Applications Center at Offutt AFB.**Background**
General Dwight D. Eisenhower commissioned the Constant Phoenix program on Sept. 16, 1947, when he charged the Army Air Forces with the overall responsibility for detecting atomic explosions anywhere in the world. In September 1949, a WB-29 flying between Alaska and Japan detected nuclear debris from Russia's first atomic test--an event thought not possible until mid-1950.
Beginning in August 1950, WB-50 aircraft were converted for the air-sampling mission over a two-year period. WC-135 aircraft began replacing the WB-50s in December 1965 and became the workhorse of the atmospheric collection program.
Air sampling missions were routinely conducted over the Far East, Indian Ocean, Bay of Bengal, Mediterranean Sea, the Polar regions, and off the coasts of South America and Africa. The WC-135W played a major role in tracking radioactive debris from the Soviet Union's Chernobyl nuclear plant disaster. 
Currently the air-sampling mission supports the Limited Nuclear Test Ban Treaty of 1963, which prohibits any nation from above ground nuclear weapons testing.  WC-135s are currently the only aircraft in the inventory conducting air-sampling operations.**General Characteristics****Primary function:** Air sampling and collection operations**Contractor:** Boeing Aerospace Co.**Power Plant:** **WC-135C**, Four Pratt & Whitney TF33-P9 turbofans without thrust reversers;**WC-135W**, Four Pratt & Whitney TF33-P-5 turbofans with thrust reversers**Thrust:** 16,050 pounds each engine**Wingspan:** 130 feet, 10 inches  (39.8 meters)**Length:** 139 feet, 11 inches  (42.5 meter)**Height:** 42 feet (12.8 meters)**Weight:** 120,170 pounds (54,508 kilograms)**Maximum Takeoff Weight:** 300,500 pounds (136,304 kilograms)**Fuel Capacity:** 130,000 pounds (58,967 kilograms)**Speed:** 403 miles per hour (350 knots)**Ceiling:** 40,000 feet  (12,192 feet)**Range:** 4,000 nautical miles **Crew:** Varies with mission**Unit Cost:**unavailable**Initial operating capability:** December 1965 **Inventory:** Active force, 2; ANG, 0; Reserve, 0
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