Convair YB-60

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YB-60
The Convair YB-60.jpg
YB-60 prototype, Convair B-36F in the background
General information
Type Strategic bomber
Manufacturer Convair
Statusprototype only
Primary user United States Air Force
Number built1 complete, 1 nearly complete
History
First flight18 April 1952
Developed from Convair B-36

The Convair YB-60 was a prototype heavy bomber built by Convair for the United States Air Force in the early 1950s. It was a purely jet-powered development of Convair's earlier mixed-power B-36 Peacemaker.

Contents

Design and development

The YB-60 landing at Rogers Dry Lake, California. YB-60 49-2676 left front landing AFFTCHO l.jpg
The YB-60 landing at Rogers Dry Lake, California.

On 25 August 1950, Convair issued a formal proposal for a swept-winged version of the B-36 with all-jet propulsion. The Air Force was sufficiently interested that on 15 March 1951, it authorized Convair to convert two B-36Fs (49-2676 and 49-2684) as the B-36G. Since the aircraft was so radically different from the existing B-36, the designation was soon changed to YB-60.

The YB-60 had 72% parts commonality with its piston-engined predecessor. The fuselages of the two aircraft were largely identical although the radar and bombing systems were located in a removable nose section as a result of the poor reliability of the B-36 installation. For initial flight testing a more streamlined nose with an instrumented boom was fitted; a wedge-shaped insert was added just outboard of the main landing gear to increase wing sweep and the tail surfaces were swept to match. The swept wings also used many B-36 parts. A steerable tail wheel was added to prevent the aircraft tipping backwards. It was not necessarily extended when on the ground but depended on how the aircraft was loaded. [1]

The YB-60's unofficial competitor for an Air Force contract was Boeing's B-52 Stratofortress. Convair's proposal was substantially cheaper than Boeing's, since it involved modifying an existing design rather than starting from scratch. Like the B-52, it was powered by eight Pratt & Whitney J57-P-3 turbojets mounted in pairs in four pods suspended below the wing. Prior to this engine configuration Convair had evaluated a six-turboprop design and one with 12 J47 engines. [2]

The first YB-60 prototype's crew numbered five; the second prototype's numbered nine, as it did in the planned production B-60s. Production B-60s were to have defensive armament similar to those of the B-36. [3]

The Convair YB-60, bearing serial number 49-2676, conducted its inaugural flight on April 18, 1952, under the command of Beryl Erickson. However, the Boeing YB-52 had beaten the Convair aircraft into flight by three days. The YB-60 was notably slower than the YB-52, cruising at about 100 mph (160 km/h) less, and encountered significant handling issues attributed to controls designed for slower speeds. Despite boasting a heavier bomb capacity—72,000 lb (33,000 kg) compared to the YB-52's 43,000 lb (20,000 kg)—the Air Force deemed the YB-60's drawbacks outweighed the benefits of its increased payload. Modifications to the B-52, such as the "big belly" configuration, eventually raised its bomb load to 60,000 lb (27,000 kg). The flight test programs for the YB-60 were terminated on January 20, 1953, having accumulated 66 flying hours. While a second prototype was nearing completion, it never had its engines installed nor its other equipment fully integrated. Despite these challenges, Convair successfully fulfilled its prototype contract, leading to the formal acceptance of both YB-60s by the Air Force in 1954. Neither operational aircraft flew again, and both airframes were dismantled and scrapped by July.

The program cost was $14.3 million. [4]

An airliner adaptation of the YB-60 was proposed by Convair, but its wingspan and weight would have required unacceptable airport infrastructure changes beyond those required for the upcoming Boeing 707. The company decided to pursue the Convair 880 series airliner instead. [5]

Specifications (YB-60)

3-view line drawing of the Convair YB-60 Convair YB-60 3-view line drawing.png
3-view line drawing of the Convair YB-60

Data from [6] [7]

General characteristics

Performance

Armament

See also

Related development

Aircraft of comparable role, configuration, and era

Related lists

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References

  1. Jenkins, pp. 190, 201
  2. Jenkins, p. 188
  3. Jenkins
  4. Knaack
  5. Jenkins, p. 201
  6. 1 2 "Convair YB-60".
  7. "Convair YB-60". Goleta Air & Space Museum. Retrieved 6 March 2022.
  8. Lednicer, David. "The Incomplete Guide to Airfoil Usage". m-selig.ae.illinois.edu. Retrieved 16 April 2019.
  9. GASM page lists 410,000 lb gross weight.
  10. GASM page data provides max wing loading = 78.3 lb/sqft.