Documents / FOIA release

The Central Intelligence Agency and Overhead Reconnaissance; the U-2 and Oxcart Programs, 1954-1974

Central Intelligence Agency · 1900-01-01 · 406 pages · text by OCR

This is a 1992 CIA History Staff monograph by Gregory W. Pedlow and Donald E. Welzenbach, originally classified Secret NOFORN and approved for release in 2013. It covers the CIA's manned overhead reconnaissance program from 1954 to 1974 and the two aircraft it developed, the U-2 and the A-12 OXCART. The history covers the U-2 overflights of the Soviet Union, the 1960 downing of Francis Gary Powers and later operations in Asia and Latin America. It also includes a section on U-2s, UFOs and Operation BLUE BOOK.

  • p. 18 …This search soon led him to a British twin-engine medium bomber—the Canberra—built by…
  • p. 19 Secret NOFORN Chapter 1 6 RAF Canberra Mark-PR3 division in Baltimore, headed by Lt. Col…
  • p. 22 …high-altitude performance of the B-57 Canberra. By January 1954 all three firms had submitted…
  • p. 36 …The RAF equipped the new Canberra PR7 with RollsRoyce Avon-109 engines and gave it long…
  • p. 37 …altitude flight being made to the US Canberra, the B-57. $ ^{41} $ ## The Intelligence Systems Panel…
  • p. 80 …production was needed to power specially configured Canberra RB-57Ds for the Air Force. The first…
  • p. 122 …a reconnaissance version of the twin-engine Canberra bomber, similar to the RAF overflight of Kapustin…
  • p. 175 …2 and an Air Force RB-57D Canberra. The two aircraft cruised along the Soviet border…
  • p. 372 …310, 313, 321, 327, 329, 332, 333 Canberra 5, 9, 23-24, 67, 109, 117, 162…
  • p. 401 …General 61 oxygen mask 62 RB-57D Canberra 162 Third Air Force 89 US deterrent force…
gravity (g's) instead of the military specification strength of 5.33 g's. For the power plant he selected the General Electric J73/GE-3 nonafterburning turbojet engine with 9,300 pounds of thrust (this was the same engine he had chosen for the F-104, which had been the basis for the U-2 design). $ ^{14} $ Many of the CL-282's design features were adapted from gliders. Thus, the wings and tail were detachable. Instead of a conventional landing gear, Johnson proposed using two skis and a reinforced belly rib for landing—a common sailplane technique—and a jettisonable wheeled dolly for takeoff. Other features included an unpressurized cockpit and a 15-cubic-foot payload area that could accommodate 600 pounds of sensors. The CL-282's maximum altitude would be just over 70,000 feet with a 2,000-mile range. Essentially, Kelly Johnson had designed a jet-propelled glider. $ ^{15} $

Early in March 1954, Kelly Johnson submitted the CL-282 design to Brig. Gen. Bernard A. Schriever's Office of Development Planning. Eugene Kiefer and Bud Wienberg studied the design and recommended it to General Schriever, who then asked Lockheed to submit a specific proposal. In early April, Kelly Johnson presented a full description of the CL-282 and a proposal for the construction and maintenance of 30 aircraft to a group of senior Pentagon officials that included Schriever's superior, Lt. Gen. Donald L. Putt, Deputy Chief of Staff for Development, and Trevor N. Gardner, Special Assistant for Research and Development to the Secretary of the Air Force. Afterward Kelly Johnson noted that the civilian officials were very much interested in his design but the generals were not. $ ^{16} $

The CL-282 design was also presented to the commander of the Strategic Air Command (SAC), Gen. Curtis E. LeMay, in early April by Eugene Kiefer, Bud Wienberg, and Burton Klein from the Office of

Kelly Johnson

Not linked to a story yet.

About this file

FOIA release, from the cia-readingroom collection. The PDF is mirrored here; the original link is under it. The text was read from the page images by an OCR model; expect the odd misread word. 406 pages are in the text index: search them above, or from the library's search.