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CIA/CSI/ History Staff Monograph, The Central Intelligence Agency and Overhead Reconnaissance: The U-2 and Oxcart Programs, 16 July 2002.

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

This is a CIA History Staff monograph by Gregory W. Pedlow and Donald E. Welzenbach, written in 1992 and approved for release in 2011. It covers the CIA's manned overhead reconnaissance program from 1954 to 1974 and its two aircraft, the U-2 and the A-12 OXCART. It follows their development, the overflights of the Soviet Union, the downing of Francis Gary Powers in 1960, and later operations. One section is titled "U-2s, UFOs, and Operation BLUE BOOK."

  • p. 4 …Scientists and Overhead Reconnaissance 17 The BEACON HILL Report 17 Concern About the Danger of a…
  • p. 14 …view of the "other side of the hill." With the advent of dry film, it became…
  • p. 30 …of this new advisory body." The BEACON HILL Report In 1951 the Air Force sought even…
  • p. 31 …Their head- quarters was located over a secretarial school on Beacon Hill, which soon became the…
  • p. 32 …to implement the ideas of the BEACON HILL Report until the summer of 1953. By this…
  • p. 34 …Created in July 1953, the Intelligence Systems Panel (ISP) included several experts from the BEACON HILL…
  • p. 37 …reconnais- sance needs expressed in the BEACON HILL Report. Theoretically, he explained to the panel, any…
  • p. 41 …H. T. Friis R. Mettler A. G. Hill E. Purcell W. H. Radford E. H. Plesset…
  • p. 44 …6(dli1i>10<25Yrs since the BEACON HILL and Intelligence Systems Panel meetings. (Si James Baker…
  • p. 45 …Having participated in the BEACON HILL Study and the Intelligence Systems Panel, several Project Three members…
  • p. 344 …He headed the Beacon Hill Panel in 1952 and later became director of Lincoln Laboratories. PARANGOSKY…
  • p. 345 …of several advisory panels, including the BEACON HILL project. He helped Baker decide what cameras to…
  • p. 364 …BEACON HILL Report: Problems of Air Force Intelligence and Reconnaissance. Massachusetts Institute of Technology, 15 June…
Chapter 6
277
CO5653421 UNCLASSIFIED
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 lift 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 models the fillets were made from electri-
cally resistive honeycomb plastic with a glass-fiber surface that
would not melt at hi g h 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 triangu-
lar shapes, known as win g 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-12'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 nonmetallic materials. Once these changes
were completed, the only metal in each vertical stabilizer was a stain-
less steel pivot. The Air Force, which later ordered several versions of
the OXCART aircraft for its own use. never adopted the laminated
vertical stabilizers.'4
THE OXCART CONTRACT
By mid-January 1960, Lockheed had demonstrated that its 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 attain
the penetration altitude he had promised to President Eisenhower.
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, "Development of Lockheed SR-71," pp. 6-7; OSA History. chap. 20, p. 35 (TS
Codeword).
UNCLASSIFIED

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FOIA release, from the cia-readingroom 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.