“Lockheed”60+ pages
- p. 4 …8
Lockheed CL-282 Supporters and the CIA. ........................................ 13
Scientists and Overhead Reconnaissance ............................................... 17
The BEACON…
- 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
(l 983).
There has also been…
- p. 22 …Immediately after returning to California, Carter proposed to
Lockheed Vice President L. Eugene Root (previously the…
- p. 23 10
Secret ld0F8RN
Chapter 1
Lockheed also submit a design. Carter noted that the proposed aircraft…
- p. 24 …who then asked Lockheed to Kelly Johnson
. sμbmit a specific proposal. In early April, Kelly Johnson…
- p. 25 .
12
Sec,et NOFORN
Chapter 1
The Lockheed CL-282 Development Planning. According to Wienberg, General…
- p. 26 …Despite the Air Force's selection
of the X-16, Lockheed continued to work on the…
- p. 27 …Proposals for special reconnaissance aircraft have been re
ceived in the Air Staff from Lockheed. Fairchild…
- p. 28 …range are not as good as the
Lockheed CL-282. :;
Gardner's enthusiasm for the CL…
- p. 29 …Few detaiils about Dulles's precise attitude
toward the proposed Lockheed reconnaissance aircraft are available,
but…
- p. 37 …for Philip Strong of the CIA had told him that the
Lockheed Aircraft Corporation had designed…
- p. 39 …Thus, even though
the Lockheed CL-282 had several important sources of support by
September I954…
- p. 40 …Council.'A
Project Three Support for the Lockheed CL-282
Chapter 1
James R. Killian, Jr…
- p. 42 …Agency.~·1
Land learned the details of Lockheed's proposed CL-282 aircraft
soon after he…
- p. 43 30
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Chapter 1
briefly mention a Lockheed design for a high-flying aircraft…
- 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 Decembeli, they
' Although the Lockheed CL-282 was not designated as the U…
- p. 53 …r the airframes to be built by Lockheed. His query was
greeted with silence. Everyone present…
- p. 55 …This category in
cluded maintenance and support personnel from Lockheed (five per
aircraft), the pilots, and…
- p. 56 …to be
settled, including the contract with Lockheed. Nevertheless. work on
the U-2 began as…
- p. 57 …A general contractor such as Lockheed
can purchase much, if not all, of the supplies needed…
- p. 58 …During the final contract negotiations in the spring
of 1958, Lockheed and the US Government agreed…
- p. 59 …Aircraft," 9 Dc:cc:mbc:r 195-i.
Lockheed Contract Filc:s. OSA Records (S ).
SeeFet
- p. 61 …F. Boc:hrne. Summary Report:
Reconnaissance Aircraft. Lockheed Aircraft Corpor.ition Report I04'.!0. 28 January…
- p. 63 …1954, even before the CIA adopted
the Lockheed proposal. Baker quickly recognized, however, that he
would…
- p. 69 …1-2 (TS Codeword); Miller, Lockheed U-2. pp. 19-20.
Sea,at
- p. 70 …By July 1955 the base
was ready, and Agency, Air Force, and Lockheed personnel began
moving…
- p. 74 61
project-the construction and testing of the aircraft-remained the ex
clusive province of Lockheed…
- 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.
10 Donald E. Welzenbach, 14 March 1986 (U): Miller…
- p. 84 …7 (TS Codeword); Miller, Lockheed U-2, p. 22.
"' OSA Hiswry, chap. 8, pp. 12-14…
- p. 85 …how to transfer Lockheed employees
from Burbank to Area 5 l without arousing a great deal…
- p. 88 …Colonel Yancey was in charge of six SAC 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 tesi: pilot
Robert Sieker 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 …After a series of tests over Edwards AFB, Lockheed began coating
the U-2s with a…
- p. 188 …Although it had been refurbished by
Lockheed and now had the more powerful 175 engine that…
- p. 199 …In the meantime Pow1ers began working for Lockheed
as a U-2 pilot. In March 1963…
- p. 200 …Beschloss claims that Powers was tired by Lockheed
for criticizing the Agency in his memoirs (which…
- p. 209 …2
One week later Colonel Geary called to order Lockheed to up
grade six older U…
- 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 …for Detachment C
Late in l 958, Lockheed began refitting the Agency's 13 remaining
U…
- p. 235 …STPOLLY
added the more advanced Lockheed P3A in 1963. Between 1955 and
1967, when the CIA…
- p. 236 …U-2 missions, and the Air Force, which had
Lockheed P-2V7 and P3A
reconnaissance aircraft
- p. 238 …The planes were maintained by Lockheed mechanics under con
tract to the CIA. The Agency attempted…
- p. 255 …All Air Force and CIA U-2s were or
dered back to Lockheed for ultrasonic inspection…
- p. 260 …The Agency dispatched several pilots to Taiwan under the cover
of Lockheed employees working on a…
- p. 264 …G in California-with three more at Lockheed undergo
ing repair. The Agency had originally ordered…
- p. 265 …Francis Gary Powers was one of the Lockheed test pilots who
checked out this new aircraft…
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
airp~ane. 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
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