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CIA-UAP-003, The Central Intelligence Agency and Overhead Reconnaissance; The U-2 and OXCART Programs, 1954-1974

Central Intelligence Agency · 1954 · 406 pages · text from the file's own layer

This is a Secret History Staff monograph by Gregory W. Pedlow and Donald E. Welzenbach of the Central Intelligence Agency, published in 1992. It gives a history of the CIA's manned overhead reconnaissance program from 1954 to 1974, covering the development and operation of the U-2 and the A-12 OXCART aircraft. It covers overflights of the Soviet Union, the 1960 downing of Francis Gary Powers, and later operations. One section is titled "U-2s, UFOs, and Operation BLUE BOOK."

From the source:Release of 2026-06-12 This CIA History Staff document chronicles the complete history of the U-2 and OXCART (A-12) high-altitude reconnaissance aircraft programs from 1954 to 1974, detailing their development, operations over the Soviet Union and other targets worldwide, the famous downing of Francis Gary Powers in 1960, organizational reforms following that incident, and the eventual transfer of operations from CIA to Air Force control. A more redacted version of this document has been available on CIA's public website.

  • p. 9 …The struggle between the CIA and the US Air Force to control the U-2 and…
  • p. 72 …2 missions. Access to the photographs taken by the U-2 would be strictly controlled, which…
  • p. 73 …This pact gave the Air Force responsibility for pilot selection and training, weather information, mission plotting…
  • p. 81 …Before the start of a mission, the ground crew set the counters to indicate the total…
  • p. 96 …All of the products from this project would be placed in the new control sys tem…
  • p. 100 …This was an S-band radar used by Soviet forces for early warning and ground-controlled…
  • p. 113 …The President nevertheless maintained tight control over the program and authorized only 10 days of overflights…
  • p. 128 …following day, when the next U-2 mission f m the Middle East. After quickly developing…
  • p. 140 …Welzenbach (S); Mission folder 4020 ( 18 March 1957), OSA records, job 67-B-972, box 7…
  • p. 142 …where they would not interfere with the control surfaces. At the ends of these poles, completely…
  • p. 147 …To take ad vantage of these weaknesses, Detachment C staged three missions from Alaska into the…
  • p. 156 …After these missions, penetrat ion overflights became a rarity. There would be only six more during…
  • p. 167 …U-2 missions. To handle U-2 material, the British created a new control system, which…
  • p. 168 …The British missions would be operationally controlled by CIA project headquarters. Soon afterward four British pilots…
  • p. 169 …where the United Kingdom carried out 27 missions during the two years its pi lots took…
  • p. 170 157 Sec, et MOF'ORI\I Chapter 3 May 1959, and used to fly weather missions…
  • p. 180 …The excellent photography from tnis mission did not reveal a single missile site, but analysts diid…
  • p. 188 …some Soviet airborne-missile fire-control systems. Operation GRAND SLAM, mission 4154 and the 24th deep…
  • p. 191 …key project personnel assembled in the Agency control center that morning (with the exception of Bissell…
  • p. 196 …in cor respondence with Abel's "wife., (probably his Soviet control) in East Germany. In November…
  • p. 204 …in .the DDP in order to maintain control of his overhead reconnais sance projects (the U…
  • p. 220 …Strongly favoring Air Force control of the U-2 missions over Cuba. the DOD representatives called…
  • p. 237 …In reality, however, the United States would maintain strict control over the missions to be flown…
  • p. 335 …The flood of information that the U-2 missions gathered led to a major expansion of…
  • p. 340 …In 1959 Bissell became Deputy Director for Plans but kept the reconnaissance projects under his control…
  • p. 348 …System-I used S- and X-band ELINT receivers to collect ground-controlled intercept and air…
  • p. 400 387 Sec1 et NOFORN mission 2023 108 mission 2029 124 mission 3086 200 mission 3088 200…
277
Seeret NOFORN
Chapter 6
eventually to the fuselage itself, creating what is known as a chine on
each side. At first Johnson was concerned that these additions might
impair the airworthiness of the plane, but wind tunnel testing deter
mined that the chines actually imparted a useful aerodynamic I ift to
the vehicle. Because titanium was very brittle and therefore difficult
to bend, Johnson achieved the necessary curvature by combining tri
angular-shaped pieces of titanium called fillets. These fillets were
glued to the framework of the chines with a special adhesive, epoxy
resin .
On later OXCART modds the fillets were made from electri
cally resistive honeycomb plastic with a glass-fiber surface that
would not melt at high speed. When struck by a radar pulse, the com
posite chines tended to absorb the pulse rather than reflect it. A simi
lar approach was used for the leading edges of the wings. Again
electrically resistive honeycomb material was fabricated into tn.J1ngu
lar shapes, known as wing teeth, and fitted into the titanium wings.
Both the metal and composite fillets and teeth were held in place with
the newly developed epoxy cements.
_. The greatest remaining area of concern in the A- l 2's radar cross
section was the two vertical stabilizers. To reduce radar ·reflections,
Kelly Johnson canted the stabilizers inward 15° and fabricated 'them
out of resin-impregnated nonmetall ic materials. Once these changes
were completed, the only metal in each vertical stabilizer was a s.tain
less steel pivot. The Air Force, which later ordered several versions of
the OXCART aircraft for its own use. never adopted the laminated
vertical stabii izers."
THE OXCART CONTRACT
By mid-January 1960, Lockheed had demonstrated that i ts concept of
shape, fuel additive, and nonmetallic parts would reduce the
OXCART's radar cross section substantially. Richard Bissell, howev
er. was very upset to learn that the changes had led to a reduction in
the aircraft's performance. which meant it would not be able to aiuain
the penetration altitude he had promised to President Eise nhower.
Kelly Johnson then proposed to reduce the aircraft's weight by 1,000
pounds and increase the fuel load by 2.000 pounds, making it possible
"Johnson. ··D,: veloprnc:n1 of Lo<:khcci.l SR-71 : · pp. 6-7: OSr\ Hiswry. chap. '.!O. p. ~;5 (TS
Codeword).
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Official release, from the pursue collection. The PDF is mirrored here; the original link is under it. 406 pages are in the text index: search them above, or from the library's search.