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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. 24 …Instead of a conventional landing gear, Johnson proposed using two skis and a reinforced belly rib…
  • p. 25 …a perceived shortcoming of the Lockheed design." Another factor in the rejection of Kelly Johnson's…
  • p. 26 …19 On 7 June 1954, Kelly Johnson received a letter from the Air Force rejecting the…
  • p. 27 …Gardner described Kelly Johnson's proposal and showed the drawings to Strong. After this meeting. Strong…
  • p. 30 …To make Kelly Johnson' s revolutionary design a reality, one addit ional source of support was…
  • p. 42 …it. A lthough Land had heard Allen Donovan '' James R. Killian. Jr.. interview by Donald E…
  • p. 48 …do the job in Johnson's airplane. And further, I overlaid a curve showing that with…
  • p. 57 …demanding, and Kelly Johnson agreed that such a move would save a lot of money. Lockheed…
  • p. 58 …Ben A. Rich (current head of the "Skunk Works"). interview by Donald E. Welzenbach and Gregory…
  • p. 69 …staff) flew over Nevada with Kelly Johnson in a small Beechcraft plane piloted by Lockheed's…
  • p. 72 …This responsibility has placed a heavy burden on the Office of Security for establishing procedures to…
  • p. 79 …Battin suggested the method used by Nazi war criminal Hermarnn Goering, a thin glass ampule containing…
  • p. 81 …Kelly Johnson used a '·wet-wing" design for the U-2, which meant that fuel was…
  • p. 89 …Airspeed was such a critical factor that Kelly Johnson added a vernier adjustment to the throttle…
  • p. 162 …By late 1957, Johnson agreed that something had to be done. After a series of tests…
  • p. 276 …The committee examined two other Kelly Johnson designs at this meeting-a tailless subsonic aircraft with…
  • p. 324 …OXCART did win a temporary reprieve in late November 1967. The Johnson administration decided to keep…
Secret i<JOFOHl'iJ
Chapter 6
278
to achieve the desired target altitude of 91,000 feet. Afterward. he
noted in the project log: ··we have no performance margins left; so
this project. instead of being 10 times as hard as anything we have
done, is 12 times as hard. This matches the design number and is ob
viously right." ,,,
These changes satisfied Bissell, who notified Johnson on 26
January that the CIA was authorizing the construction of 12 of the
new aircraft. The actual contract was signed on 11 February l 960.
Lockheed's original quotation for the project was $96.6 million for l 2
aircraft, but technological difficulties eventually made this price im
possible to meet. Recognizing that fabricating an aircraft from tita
nium might involve unforeseen difficulties, the CIA included a clause
in the contract that allowed costs to be reevaluated. During the next
five years. this clause had to be invoked on a number of occasions as
the A-12's costs soared to more than double the original estimate."'
NEW TECHNOLOGIES NECESSITATED
BY OXCART'S HIGH SPEED
According to the specifications. the OXCART aircraft was to achieve
a speed of Mach 3.2 (2.064 knots or 0.57 miles per second. which
would make it as fast as a rifle bullet). have a range of 4.120 nautical
miles. and reach altitudes of 84.500 to 97,600 feet. The new aircraft
would thus be more than five times as fast as the U-2 and would go
almost 3 miles higher.
One major disadvantage of the OXCART's great speed was high
temperatures. Flying through the earth's atmosphere at Mach 3.2
heated portions of the aircraft's skin to almost 900°F. An aircraft op
erating at these high speeds and high temperatures required fuels. lu
bricants, and hydraulic fluids that had not yet been invented. The
OXCART's fuel requirement called for a low-vapor-pressure fuel
with a low volume at operating temperatures; the fuel would also be
used as a heat sink to cool various parts of the aircraft. The 158 en
gines required lubricants that did not break down at the very high op
erating temperatures of Mach 3.2 speeds. This requirement led to the
,., Johnson... Archangc I log," 2 I January I960.
'" OSA Hiswry. chap. 20. pp. 27-29. 33-34, 36 (TS Colkword).
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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.