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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. 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…
CO5653421 UNCLASSIFIED
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Chapter 2
68
power-to-weight ratio of 2.7: I was almost 20 percent less efficient
than the preferred P-31 version.'
To conduct lengthy missions over hostile territory, the U-2
needed to carry a large amount of fuel. Kelly Johnson used a
"wet-wing" design for the U-2, which meant that fuel was not stored
in separate fuel tanks but rather in the wing itself. Each wing was di-
vided into two leak-proof compartments, and fuel was pumped into
all the cavities within these areas; only the outer 6 feet of the wings
were not used for fuel storage. The U-2 also had a 100-gallon reserve
tank in its nose. Later, in 1957, Johnson increased the fuel capacity of
the U-2 by adding 100-gallon -slipper" tanks under each wing, pro-
jecting slightly ahead of the leading edge.
One of the most important considerations in the U-2's fuel sys-
tem was the need to maintain aircraft trim as the fuel was consumed.
The aircraft therefore contained a complex system of feed lines and
valves draining to a central sump, which made it impossible to pro-
vide the pilot with an empty/full type of fuel gauge. None of the first
50 U-2s had normal fuel gauges. Instead there were mechanical fuel
totalizer/counters. Before the start of a mission, the ground crew set
the counters to indicate the total amount of fuel in the wings. and then
a flow meter subtracted the gallons of fuel actually consumed during
the flight. The pilot kept a log of the fuel consumption shown by the
counters and compared it with estimates made by mission planners
for each leg of the flight. As a double check, U-2 pilots also kept
track of their fuel consumption by monitoring airspeed and time in
the air. Most pilots became quite expert at this. Several who did not
came up short of their home base during the 20 years these planes
were flown.4'
INITIAL TESTING OF THE U-2
Preliminary taxi trials began on 27 July 1955, when the first run down
the newly completed runway took the plane to 50 knots. Lockheed's
chief test pilot, Tony LeVier, was at the controls. A second taxi trial
OSA Hiswry, chap. 8. p. 13 (TS Codewort).
Information supplied by Norman Nelson. former director of Lockheed's Skunk Works,
to Donald E. Welzenbach, 14 March 1986 (U): Miller. Lockheed U-2. pp. 77, 96.
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.