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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…
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Chapter 2
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followed on I August. LeVier accelerated to 70 knots and began to try
the ailerons. "It was at this point that I became aware of being air-
borne." LeVier noted afterward, -which left me with utter amaze-
ment, as I had no intentions whatsoever of flying. I immediately
started back toward the ground, but had difficulty determining my
height because the lakebed had no markings to judge distance or
height. I made contact with the ground in a left bank of approximately
10 degrees." The U-2 bounced back into the air, but LeVier was able
to bring it back down for a second landing. He then applied the brakes
with little effect, and the aircraft rolled for a long distance before
coming to a stop."
Bissell, Cunningham. and Johnson saw the aircraft fall and
bounce. Leaping into a jeep, they roared off toward the plane. They
signaled to LeVier to climb out and then used fire extinguishers to put
out a tire in the brakes. At a debriefing session that followed. LeVier
complained about the poor performance of the brakes and the absence
of markings on the runway. Damage to the prototype U-2 was very
minor: blown tires, a leaking oleostrut on the undercarriage, and dam-
aged brakes. This unplanned flight was but a foretaste of the airwor-
thiness of the U-2. New pilots all had difficulty in getting the U-2's
wheels on the ground because at low speeds it would remain in
ground effect and glide effortlessly above the runway for great dis-
tances.
Taxi trials continued for one more day and were followed by the
first planned flight on 4 August 1955. LeVier was again at the con-
trols and had been instructed by Kelly Johnson to land the U-2 by
making initial contact with the main or forward landing gear and let-
ting the plane settle back on the rear wheel. LeVier had disagreed
with this approach. believing that the U-2 would bounce if he tried to
touch down on the forward gear first. After flying the aircraft up to
8,000 feet, LeVier leveled off and began cycling the landing gear up
and down: then he tested the flaps and the plane's stability and control
systems. Finally. LeVier made his first landing approach. As the U-2
settled down, the forward landing gear touched the runway and the
plane skipped and bounced into the air. LeVier made a second attempt
to land front wheels first, and again the plane bounded into the air.
Transcripts of the test pilots and observers' comments on the initial U-2 test tlights
have been published in "Secret First Flight of Article 001," Spyp/anes vol. 2, 1988, pp.
64-71. 82-85.
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.