“Lockheed”60+ pages
- p. 4 …Search for a New Reconnaissance Aircraft 8
Lockheed CL-282 Supporters and the CIA 13
Scientists…
- p. 6 …260
Competition Between Lockheed and Convair 267
The Selection of the Lockheed Design 270
Efforts To…
- p. 12 …excellent technical study of the U-2: Lockheed U-2
(1983).
E0129581.131d111>10<25Yrs…
- p. 21 …August 1953, OS1 records (S).
" Jay Miller, Lockheed U-2, Aerograph 3 (Austin, Texas: Aerofax, 1983…
- p. 22 …Immediately after returning to California, Carter proposed to
Lockheed Vice President L. Eugene Root (previously the…
- p. 23 …high-altitude
reconnaissance aircraft
Chapter 1
10
Lockheed also submit a design. Carter noted that the…
- p. 24 …Miller, Lockheed U-2, p. 12. For more details on Kelly Johnson's original proposal.
see…
- p. 25 12
The Lockheed CL-282
CO5653421 UNCLASSIFIED
Chapter 1
Development Planning. According to Wienberg, General LeMay…
- p. 26 …Despite the Air Force's selection
of the X-16, Lockheed continued to work on the…
- p. 27 …six days before the Wright Air Development Command
began to evaluate the Lockheed proposal. Gardner described…
- p. 28 …range are not as good as the
Lockheed CL-282.
Gardner's enthusiasm for the CL…
- p. 29 …Few details about Dulles's precise attitude
toward the proposed Lockheed reconnaissance aircraft are available,
but…
- p. 30 …At this point, the summer of 1954, Lockheed's CL-282 proposal
still lacked official support…
- p. 37 …ISP chairman Baker then urged Donovan to travel to
southern California to evaluate the Lockheed design…
- p. 39 …Thus, even though
the Lockheed CL-282 had several important sources of support by
September 1954…
- p. 40 …Council.46
Project Three Support for the Lockheed CL-282
Even before the final Technological Capabilities…
- p. 42 …Agency.49
Land learned the details of Lockheed's proposed CL-282 aircraft
soon after he…
- p. 43 …Chapter 1
30
briefly mention a Lockheed design for a high-flying aircraft at the
24…
- p. 44 …During September and October the Project Three study group
met frequently to discuss the Lockheed design…
- p. 47 …The Lockheed super glider will fly at 70,000 feet, well out of the
reach of…
- p. 48 …Putt, to oppose the adoption of the Lockheed design. The officials ar-
gued that the Bell…
- p. 49 …He used Gardner's
statement to convince Lockheed's senior management to approve the
project, which…
- p. 50 …small group of prominent scientists that the
Lockheed design represented the best possible overhead reconnais-
sance…
- p. 52 …afternoon of 3 December, they
Although the Lockheed CL-282 was not designated as the U…
- p. 53 …Eventually Bissell asked who was
going to pay for the airframes to be built by Lockheed…
- p. 55 …This category in-
cluded maintenance personnel from Lockheed (five per
aircraft), the pilots, and support personnel…
- p. 57 …Then on 22 December 1954, the Agency
signed a letter contract with Lockheed, using the codename…
- p. 58 …The U-2 would have a
The Lockheed "Skunk Works" was named after the Kickapoo Joy…
- p. 59 …Johnson, -A High-Altitude Reconnaissance Aircraft, - 9 December 1954,
Lockheed Contract Files, OSA Records (S).
UNCLASSIFIED
- p. 61 …Reconnaissance Aircraft, Lockheed Aircraft Corporation Report 10420. 28 January 1955.
pp. 7-9, OSA Recordsi \ (5…
- p. 63 …1954, even before the CIA adopted
the Lockheed proposal. Baker quickly recognized, however, that he
would…
- p. 69 …Miller, Lockheed U-2. pp. 19-20.
Sè'biet
UNCLASSIFIED
- p. 74 …aircraft—remained the ex-
clusive province of Lockheed:9
As a result of this agreement, CIA…
- p. 77 …The first model of the
pressure suit, used by Lockheed test pilots, made no provision for…
- p. 79 …Geary told Culbertson that the Lockheed
CL-282 was going to be known officially as the…
- p. 81 …former director of Lockheed's Skunk Works,
to Donald E. Welzenbach, 14 March 1986 (U): Miller…
- p. 84 …7 (TS Codeword); Miller, Lockheed U-2, p. 22.
OSA History, chap. 8, pp. 12-14…
- p. 85 …how to transfer Lockheed employees
from Burbank to Iwithout arousing a great deal of curiosity.
The…
- p. 88 …Colonel Yancey was in charge of six SAL pilots who were to be
trained by Lockheed…
- p. 90 …CIA, which then placed an order with
Lockheed for 29 U-2s in configurations to be…
- p. 107 …U-2
cover story stating that a Lockheed-developed aircraft would be flown
by the USAF…
- p. 143 …Lockheed mechanics
had mounted the various RAINBOW devices on the prototype U-2, a
Lockheed test…
- p. 144 …Unable to restart the power plant, Lockheed test pilot
Robert Sicker bailed out but was struck…
- p. 145 …The loss of one of Lockheed's best test pilots, as well as the pro-
totype…
- p. 157 …As a substitute,
Lockheed began working to develop a paint with radar-suppressant
qualities, but this…
- p. 162 …a series of tests over Edwards AFB. Lockheed began coating
the 11-2s with a standard…
- p. 188 …Although it haL refurbished by
Lockheed and now had the more powerful 175 engine that would…
- p. 200 …Beschloss claims that Powers was fired by Lockheed
for criticizing the Agency in his memoirs (which…
- p. 209 …Some poetic justice in this.'
One week later Colonel Geary called to order Lockheed to up…
- p. 211 …In May 1961, Lockheed began modifying Agency U-2s so that
they could be refueled in…
- p. 220 …story, which
was that its pilots were Lockheed employees on a ferry flight to
Puerto Rico…
- p. 230 …CO5653421 UNCLASSIFIED
Chapter 5
Late in 1958, Lockheed began refitting the Agency's 13 remaining
U…
- p. 264 …1966 decided to place an order with Lockheed for ei g ht more aircraft
to be…
- p. 265 …Francis Gary Powers was one of the Lockheed test pilots who
checked out this new aircraft…
- p. 266 …began coming off the production line at Lockheed
in-the autumn of 1968, CIA and the…
- p. 273 …SP-1362, "History of the OXCART Program,"
Lockheed Aircraft Corporation, Burbank, CA. 1 July 1968, p…
- p. 275 …Personnel at Lockheed's Skunk Works referred to
these aircraft concepts as "Archangel-1," "Archangel-2…
- p. 276 RN
Chapter 6
263
Johnson, "Archangel log," 17-24
CO5653421 UNCLASSIFIED
Lockheed design for a hydrogen…
- p. 280 …During the first half of 1959, both Lockheed and Convair
worked to reduce the radar cross…
- p. 281 …In early June, Lockheed submitted a design for a ground-launched
aircraft known as the A…
CO5653421 UNCLASSIFIED
Secre N
Chapter 2
47
In designing the U-2 aircraft, Kelly Johnson was confronted with
two major problems—fuel capacity and weight. To achieve interconti-
nental range, the aircraft had to carry a large supply of fuel, yet, it
also had to be light enough to attain the ultrahigh altitudes needed to
be safe from interception. Although the final product resembled a typ-
ical jet aircraft, its construction was unlike any other US military air-
craft. One unusual design feature was the tail assembly, which—to
save weight—was attached to the main body with just three tension
bolts. This feature had been adapted from sailplane designs.
The wings were also unique. Unlike conventional aircraft, whose
main wing spar passes through the fuselage to give the wings continu-
ity and strength, the U-2 had two separate wing panels, which were
attached to the fuselage sides with tension bolts (again, just as in sail-
planes). Because the wing spar did not pass through the fuselage,
Johnson was able to locate the camera behind the pilot and ahead of
the engine, thereby improving the aircraft's center of gravity and re-
ducing its weight.
The wings were the most challenging design feature of the entire
airplane. Their combination of high-aspect ratio and low-,drag ratio
(in other words, the wings were long, narrow, and thin) made them
unique in jet aircraft design. The wings were actually integral fuel
tanks that carried almost all of the U-2's fuel supply.
The fragility of the wings and tail section, which were only
bolted to the fuselage, forced Kelly Johnson to look for a way to pro-
tect the aircraft from gusts of wind at altitudes below 35,000 feet,
which otherwise might cause the aircraft to disintegrate. Johnson
again borrowed from sailplane designs to devise a "gust control"
mechanism that set the ailerons and horizontal stabilizers into a posi-
tion that kept the aircraft in a slightly nose-up attitude, thereby
avoiding sudden stresses caused by wind gusts. Nevertheless, the U-2
remained a very fragile aircraft that required great skill and concen-
tration from its pilots.
The final major design feature was the lightweight, bicycle-type
landing gear. The entire structure—a single oleostrut with two light-
weight wheels toward the front of the aircraft and two small,
solid-mount wheels under the tail—weighed only 208 pounds yet
could withstand the force of touchdown for this 7-ton aircraft. Because
both sets of wheels were located underneath the fuselage, the U-2 was
also equipped with detachable pogos (long, curved sticks with two
small wheels on them) on each wing to keep the wings level during
takeoff. The pilot would drop the pogos immediately after takeoff so
UNCLASSIFIED