Documents / Official release

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. 11 …At great risk, US Air Force and Navy aircraft had been conducting peripheral reconnaissance and shallow…
  • p. 16 …As a result, in the late 1940s, the US Air Force and Navy began trying to…
  • p. 17 …Two months later, on 7 October 1952, Soviet fighter aircraft stalked and shot down a US…
  • p. 72 …The terminology used to describe U-2 aircraft and pilots also played a part in maintaining…
  • p. 94 …The committee issued its l ist of cargets for the use of the entire intelli gence…
  • p. 147 …The Agency then turned co the Navy, which granted permission for Detachmernt C to use the…
  • p. 180 …James Doolittle urged President Eisenhower to use overflights of the Soviet Union to the maximum degree…
  • p. 223 …by Air Force and Navy reconnais sance aircraft. President Kennedy used NPIC photographs to i llustrate…
  • p. 273 …Charyk, and his Navy counterpart, Garrison Norton. Designers from several air craft manufacturers also attended some…
  • p. 283 …This engine had originally been developed for the Navy's large, jet-powered flying boat, the…
  • p. 297 …The need for additional bui ldings on the base was met by the Navy. Three surplus…
  • p. 298 …After hearing Bissell and Holcomb's suggestion that the 158 might be used in future Navy…
  • p. 348 …Following modifications to make System-VII suitable for use by the Navy, the designation was changed…
  • p. 353 …In 1968 tests on an AQUILINE prototype at Randsburg Wash on the US Navy's Naval…
  • p. 401 …247, 328 US Marine Corps Reserve 14 US Military Academy at West Point 329 US Navy…
25
CL-282 design was essentially a jet-propelled glider capable of attain
ing the altitudes that he felt were necessary to carry out reconnais
sance of the Soviet Union successfully:1
Upon his return east on 8 August, Donovan got in touch with
James Baker and suggested an urgent meeting of the Intelligence
Systems Panel. Because of other commitments by the members, how
ever, the panel did not meet to hear Donovan's report until 24
September 1954 at the Cornell Aeronautical Laboratory. Several
members, including Land and Strong, were absent. Those who did at
tend were upset to learn that the Air Force had funded a closed com
petition for a tactical reconnaissance plane without informing them.
But once Donovan began describing Kelly Johnson's rejected design
for a jet-powered glider, they quickly forgot their annoyance and lis
tened intently.
Donovan began by stressing that high-altitude reconnaissance
aircraft had to fly above 70,000 feet to be safe from interception.
Next, he set out what he considered to be the three essential re
quirements for a high-altitude spyplane: a single engine, a sailplane
wing, and low structural load factors. Donovan strongly favored
single-engine aircraft because they are both lighter and more reli
able than multiengine aircraft. Although a twin-engine aircraft could
theoretically return to base on only one engine, Donovan explained,
it could only do so at a much lower altitude, about 34,000 feet,
where it was sure to be shot down.
The second of Donovan's essential factors, a sailplane wing (in
technical terms a high-aspect-ratio, low-induced-drag wing). was
needed to take maximum advantage of the reduced thrust of a jet en
gine operating in the rarefied atmosphere of extreme altitude. Because
of the thinness of the atmosphere above 70,000 feet, engineers esti
mated that the power curve of a jet engine would fall off to about 6
percent of its sea-level thrust.
Finally, low structural load factors, like those used by transport
aircraft, were necessary to reduce weight and thereby achieve maxi
mum altitude. Donovan explained that strengthening wings and
" Donovan interview (S)
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Chapter 1
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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.