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/specialCollection/MissileGap/1992/1992-04-01.pdf

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, published in Washington in 1992 and approved for release in 2011. It covers the CIA's manned overhead reconnaissance program from 1954 to 1974, which developed and flew the U-2 and the A-12 OXCART. It traces the U-2's development, the overflights of the Soviet Union, the downing of Francis Gary Powers on 1 May 1960, and later operations. One section is titled U-2s, UFOs, and Operation BLUE BOOK.

  • 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 …interview by Donald E. Welzenbach, Corona del Mar. California. 20 May 1985 (S). Johnson, "Log for…
  • 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 additional source of support was necessary…
  • p. 42 …When James Killian asked Land to head Project Three, Land had to make a major decision…
  • p. 48 …do the job in Johnson's airplane. And further, 1 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 …a week after he had been authorized to begin the project, Kelly Johnson wrote a 23…
  • p. 69 …project staff) flew LIZ with Kelly Johnson in a small Beechcraft plane piloted by eed's…
  • p. 72 …This responsibility has placed a heavy burden on the Office of Security for establishing procedures to…
  • p. 79 …Batlin suggested the method used by Nazi war criminal Hermann 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 RN Chapter 6 263 Johnson, "Archangel log," 17-24 CO5653421 UNCLASSIFIED Lockheed design for a hydrogen…
  • p. 324 …OXCART did win a temporary reprieve in late November 1967. The Johnson administration decided to keep…
199
Aftermath of the Bay of Pigs
invasion, 20 April 1961
005653421 UNCLASSIFIED
Refueling a U-2 in flight was a very delicate task. When fully
loaded with fuel, KC-135 tankers found it difficult to reduce airspeed
to-200 knots, the safest speed for refueling a U-2. As for the U-2s,
they were in a very vulnerable position when approaching a tanker at
200 knots because their frail wings could not stand much stress. As a
result, U-2 pilots had to approach the KC-135 tankers very carefully
in order to avoid the vortexes from the wingtips of the tanker and the
turbulence caused by the four large jet engines. During the first few
years of refueling operations, two U-2s crashed after their wings
broke off as they crossed into the turbulent area behind the tankers;
one of the pilots was killed!'
The in-flight refueling capability was a useful modification to
the U-2, but it could not dramatically extend mission length. The
main limiting factor remained pilot fatigue, which prevented missions
from lasting longer than approximately 10 hours.
U-2 Coverage During the Cuban Missile Crisis
Cuba remained a high-priority target even after the Bay of Pigs inva-
sion failed in April 1961. Soon afterward, Detachment G U-2s began
flying monthly missions over Cuba in a program known as Project
" Ibud.. p. 11-12 (TS Codeword).
ret
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.