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 GLM-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. 22 …Air Force headquarters soon approved Martin's proposal to modify the B-57 and was very…
  • p. 31 …Their headquarters was located over a secretarial school on Beacon Hill, which soon became the codename…
  • p. 55 Secret NOFORN Chapter 2 42 The Matomic Building total of 357 personnel divided among project headquarters…
  • p. 56 …until it moved into the new CIA Headquarters building at Langley in March 1962. The final…
  • p. 73 …On 3 August 1955, Dulles and Twining met at SAC headquarters in Omaha to sign the…
  • p. 85 …Frequent flights were also necessary to bring in supplies and visitors from contractors and headquarters. Therefore…
  • p. 102 …U-2 project officer, the Air Force Headquarters project officer, and NACA's top official, Dr…
  • p. 107 …did not have to report to higher headquarters. WRSP-1, known within the Agency as Detachment…
  • p. 117 …Late on the evening of 3 July, Bissell went to project headquarters in the Matomic Building…
  • p. 127 …The PARAMOUNT Committee worked inside PID headquarters in the Steuart Building. Composed of members from CIA…
  • p. 128 …Lundahl and Reber flew from the United Kingdom to US Air Force Europe headquarters in Wiesbaden…
  • p. 138 …later and promptly reported the conversation to headquarters. When details of Vito's close call reached…
  • p. 153 …of Detachment A achieved excellent results, project headquarters had already decided that Western Europe was not…
  • p. 168 …The British missions would be operationally controlled by CIA project headquarters. Soon afterward four British pilots…
  • p. 191 …commander at Adana, to Air Force Europe headquarters, to replace the cover story that had been…
  • p. 194 …Because the new government had not been briefed on the U-2, Project Headquarters refused to…
  • p. 205 …its own building to the new CIA Headquarters at Langley. Soon afterward, Col. Stanley W. Beerli…
  • p. 233 …On 6 June 1960, project headquarters decided on a phased-out withdrawal of Detachment C between…
  • p. 235 …Airport, the pilot reported the incident to Headquarters. The Office of Security immediately contacted the Pennsylvania…
  • p. 312 …Project headquarters therefore began preparing contingency plans (Project SKYLARK) for the possible employment of OXCART over…
  • p. 319 …To ensure secure communications between Headquarters and Kadena. A typical mission over North Vietnam required refueling…
  • p. 323 …Project headquarters informed Deputy Defense Secretary Vance on 10 January 1967 that the A-12s would…
  • p. 324 …President Johnson confirmed this decision on 21 May. $ ^{69} $ Project headquarters selected 8 June 1968 as…
  • p. 334 …Air Force personnel served at all levels of the reconnaissance program, from project headquarters to the…
  • p. 365 …Speech given by Richard Bissell at CIA Headquarters, 12 October 1965 (Top Secret Codeword). Interview with…

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Secret NOFORN

power-to-weight ratio of 2.7:1 was almost 20 percent less efficient than the preferred P-31 version. $ ^{40} $

To conduct lengthy missions over hostile territory, the U-2 needed to carry a large amount of fuel. Kelly Johnson used a "wet-wing" design for the U-2, which meant that fuel was not stored in separate fuel tanks but rather in the wing itself. Each wing was divided into two leak-proof compartments, and fuel was pumped into all the cavities within these areas; only the outer 6 feet of the wings were not used for fuel storage. The U-2 also had a 100-gallon reserve tank in its nose. Later, in 1957, Johnson increased the fuel capacity of the U-2 by adding 100-gallon "slipper" tanks under each wing, projecting slightly ahead of the leading edge.

One of the most important considerations in the U-2's fuel system was the need to maintain aircraft trim as the fuel was consumed. The aircraft therefore contained a complex system of feed lines and valves draining to a central sump, which made it impossible to provide the pilot with an empty/full type of fuel gauge. None of the first 50 U-2s had normal fuel gauges. Instead there were mechanical fuel totalizer/counters. Before the start of a mission, the ground crew set the counters to indicate the total amount of fuel in the wings, and then a flow meter subtracted the gallons of fuel actually consumed during the flight. The pilot kept a log of the fuel consumption shown by the counters and compared it with estimates made by mission planners for each leg of the flight. As a double check, U-2 pilots also kept track of their fuel consumption by monitoring airspeed and time in the air. Most pilots became quite expert at this. Several who did not came up short of their home base during the 20 years these planes were flown.41

## INITIAL TESTING OF THE U-2

Preliminary taxi trials began on 27 July 1955, when the first run down the newly completed runway took the plane to 50 knots. Lockheed's chief test pilot, Tony LeVier, was at the controls. A second taxi trial

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About this file

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