Jump to content

Lockheed YF-12

From Wikipedia, the free encyclopedia

This is an old revision of this page, as edited by Gfox88 (talk | contribs) at 20:31, 14 September 2018 (Added {{convert}} tags). The present address (URL) is a permanent link to this revision, which may differ significantly from the current revision.

YF-12
YF-12A
Role Interceptor aircraft
Manufacturer Lockheed Corporation
Designer Clarence "Kelly" Johnson
First flight 7 August 1963
Status Canceled
Primary user United States Air Force
Number built 3
Developed from Lockheed A-12
Variants Lockheed SR-71 Blackbird

The Lockheed YF-12 was an American prototype interceptor aircraft evaluated by the United States Air Force. The YF-12 was a twin-seat version of the secret single-seat Lockheed A-12 reconnaissance aircraft, which led to the U.S. Air Force's Lockheed SR-71 Blackbird twin-seat reconnaissance variant. The YF-12 set and held speed and altitude world records of over 2,000 miles per hour (3,200 km/h) and over 80,000 feet (24,000 m) (later surpassed by the SR-71), and is the world's largest manned interceptor to date.[1]

Design and development

In the late 1950s, the United States Air Force (USAF) sought a replacement for its F-106 Delta Dart interceptor. As part of the Long Range Interceptor Experimental (LRI-X) program, the North American XF-108 Rapier, an interceptor with Mach 3 speed, was selected. However, the F-108 program was canceled by the Department of Defense in September 1959.[2] During this time, Lockheed's Skunk Works was developing the A-12 reconnaissance aircraft for the U.S. Central Intelligence Agency (CIA) under the Oxcart program. Kelly Johnson, the head of Skunk Works, proposed to build a version of the A-12 named AF-12 by the company; the USAF ordered three AF-12s in mid-1960.[3]

The AF-12s took the seventh through ninth slots on the A-12 assembly line; these were designated as YF-12A interceptors.[4] The main changes involved modifying the A-12's nose by cutting back the chines to accommodate the huge Hughes AN/ASG-18 fire-control radar originally developed for the XF-108, and the addition of the second cockpit for a crew member to operate the fire control radar for the air-to-air missile system. The modifications changed the aircraft's aerodynamics enough to require ventral fins to be mounted under the fuselage and engine nacelles to maintain stability. The four bays previously used to house the A-12's reconnaissance equipment were converted to carry Hughes AIM-47 Falcon (GAR-9) missiles.[5] One bay was used for fire control equipment.[6]

Lockheed YF-12A, Serial# 60-6934, the only YF-12A in ADC markings

The first YF-12A flew on 7 August 1963.[5] President Lyndon B. Johnson announced the existence of the aircraft[A][7] on 24 February 1964.[8][9] The YF-12A was announced in part to continue hiding the A-12, its still-secret ancestor; any sightings of CIA/Air Force A-12s based at Area 51 in Nevada could be attributed to the well-publicized Air Force YF-12As based at Edwards Air Force Base in California.[7]

On 14 May 1965, the Air Force placed a production order for 93 F-12Bs for its Air Defense Command (ADC).[10] However, Secretary of Defense Robert McNamara would not release the funding for three consecutive years due to Vietnam War costs.[10] Updated intelligence placed a lower priority on defense of the continental US, so the F-12B was deemed no longer needed. Then in January 1968, the F-12B program was officially ended.[11]

Operational history

Air Force testing

Sideview of black jet aircraft overflying mountain towards right of photo.
YF-12A overflying a mountain.

During flight tests the YF-12As set a speed record of 2,070.101 miles per hour (3,331.505 km/h) and altitude record of 80,257.86 feet (24,462.60 m), both on 1 May 1965,[8] and demonstrated promising results with its unique weapon system. Six successful firings of the AIM-47 missiles were completed. The last one was launched from the YF-12 at Mach 3.2 at an altitude of 74,000 feet (23,000 m) to a JQB-47E target drone 500 feet (150 m) off the ground.[12] One of the Air Force test pilots, Jim Irwin, would go on to become a NASA astronaut and walk on the Moon.

The program was abandoned following the cancellation of the production F-12B, but the YF-12s continued flying for many years with the USAF and with NASA as research aircraft.

NASA testing

NASA Overview of the YF-12, circa 1974 (26:38)

The initial phase of the test program included objectives aimed at answering some questions about implementation of the B-1. Air Force objectives included exploration of its use in a tactical environment, and how airborne early warning and control (AWACS) would control supersonic aircraft. The Air Force portion was budgeted at US$4 million. The NASA tests would answer questions such as how engine inlet performance affected airframe and propulsion interaction, boundary layer noise, heat transfer under high Mach conditions, and altitude hold at supersonic speeds. The NASA budget for the 2.5-year program was US$14 million.[13]

Of the three YF-12As, AF Ser. No. 60-6934 was damaged beyond repair by fire at Edwards AFB during a landing mishap on 14 August 1966; its rear half was salvaged and combined with the front half of a Lockheed static test airframe to create the only SR-71C.[14][15]

YF-12A, AF Ser. No. 60-6936 was lost on 24 June 1971 due to an in-flight fire caused by a failed fuel line; both pilots ejected safely just north of Edwards AFB. YF-12A, AF Ser. No. 60-6935 is the only surviving YF-12A; it was recalled from storage in 1969 for a joint USAF/NASA investigation of supersonic cruise technology, and then flown to the National Museum of the United States Air Force at Wright-Patterson Air Force Base near Dayton, Ohio on 17 November 1979.[8]

A fourth YF-12 aircraft, the "YF-12C", was actually the second SR-71A (AF Ser. No. 61–7951). This SR-71A was re-designated as a YF-12C and given the fictitious Air Force Serial Number 60-6937 from an A-12 to maintain SR-71 secrecy. The aircraft was loaned to NASA for propulsion testing after the loss of YF-12A (AF Ser. No. 60–6936) in 1971. The YF-12C was operated by NASA until September 1978, when it was returned to the Air Force.[16]

The YF-12 had a real-field sonic-boom overpressure value between 33.5 and 52.7 N/m2 (0.7 to 1.1 lb/ft2) – below 48 was considered "low".[17]

Variants

YF-12A
Pre-production version. Three were built.[18]
F-12B
Production version of the YF-12A; canceled before production could begin.[19]
YF-12C
Fictitious designation for an SR-71 provided to NASA for flight testing. The YF-12 designation was used to keep SR-71 information out of the public domain.[20]

Operators

 United States

Accidents and incidents

  • 24 July 1971 YF-12A 60-6936 (Article 1003) was lost in an accident near Edwards Air Force Base, California, United States.

Aircraft on display

YF-12A AF Ser. No. 60-6935 in the National Museum of the USAF
YF-12A

Specifications (YF-12A)

Orthographically projected diagram of the Lockheed YF-12.
Orthographically projected diagram of the Lockheed YF-12.

Data from Lockheed's SR-71 'Blackbird' Family[23]

General characteristics

  • Crew: 2; pilot and fire control officer (FCO)
  • Aspect ratio: 1.7

Performance

Armament

Avionics

  • Hughes AN/ASG-18 look-down/shoot-down fire control radar

See also

Related development

Related lists

References

Notes

  1. ^ Johnson's speech named the plane A-11, the name for the two-seat design.

Citations

  1. ^ Pace, Steve (1995). X-Planes at Edwards. p. 11. ISBN 978-1-61060786-5.
  2. ^ Pace 2004, pp. 45–46.
  3. ^ Pace 2004, pp. 46–47.
  4. ^ Landis and Jenkins 2005, pp. 40–41.
  5. ^ a b c d Green and Swanborough, 1988, p. 350.
  6. ^ "Hughes AIM-47 Falcon". Designation systems.
  7. ^ a b McIninch 1996, p. 15.
  8. ^ a b c Air Force Museum Foundation, 1983, p. 133.
  9. ^ McIninch 1996, p. 14.
  10. ^ a b Pace 2004, p. 53.
  11. ^ Donald 2003, pp. 148, 150.
  12. ^ Landis and Jenkins 2005, p. 44.
  13. ^ Drendel 1982, p. 6.
  14. ^ Landis and Jenkins 2005, pp. 62, 75.
  15. ^ Pace 2004, pp. 109–10.
  16. ^ Landis and Jenkins 2005, pp. 49–55.
  17. ^ Dugan, James F. Jr. "Preliminary study of supersonic-transport configurations with low values of sonic boom", p. 18. NASA Lewis Research Center, March 1973. Retrieved: March 2012.
  18. ^ Landis and Jenkins 2005, p. 40.
  19. ^ Landis and Jenkins 2005, p. 46.
  20. ^ Landis and Jenkins 2005, pp. 49–50.
  21. ^ "YF-12A/60-6935." Archived 4 April 2013 at the Wayback Machine National Museum of the USAF. Retrieved: 16 April 2013.
  22. ^ "YF-12A/60-6934." Archived 23 April 2013 at the Wayback Machine Hill Aerospace Museum. Retrieved: 16 April 2013.
  23. ^ Goodall and Miller, 2002.

Bibliography

  • Air Force Museum Foundation Inc. US Air Force Museum. Dayton, Ohio: Wright-Patterson AFB, 1983.
  • Donald, David, ed. "Lockheed's Blackbirds: A-12, YF-12 and SR-71". Black Jets. AIRtime, 2003. ISBN 1-880588-67-6.
  • Drendel, Lou. SR-71 Blackbird in Action. Carrollton, Texas: Squadron/Signal Publications, 1982, ISBN 0-89747-136-9.
  • Goodall, James and Jay Miller. Lockheed's SR-71 'Blackbird' Family. Hinchley, England: Midland Publishing, 2002, ISBN 1-85780-138-5.
  • Green, William and Gordon Swanborough. The Complete Book of Fighters. New York: Barnes & Noble, 1988, ISBN 0-7607-0904-1.
  • Jenkins, Dennis R. Lockheed Secret Projects: Inside the Skunk Works. St. Paul, Minnesota: MBI Publishing, 2001, ISBN 978-0-7603-0914-8.
  • Jenkins, Dennis R. and Tony R. Landis. Experimental & Prototype U.S. Air Force Jet Fighters. Minnesota, US: Specialty Press, 2008, ISBN 978-1-58007-111-6.
  • Knaack, Marcelle Size. Encyclopedia of US Air Force Aircraft and Missile Systems: Volume 1 Post-World War II Fighters 1945–1973. Washington, DC: Office of Air Force History, 1978. ISBN 0-912799-59-5.
  • Landis, Tony R. and Dennis R. Jenkins. Lockheed Blackbirds. North Branch, Minnesota: Specialty Press, revised ed., 2005, ISBN 1-58007-086-8.
  • McIninch, Thomas. "The Oxcart story". Center for the Study of Intelligence, Central Intelligence Agency, 2 July 1996. Retrieved: 10 April 2009.
  • Pace, Steve. Lockheed SR-71 Blackbird. Swindon: Crowood Press, 2004, ISBN 1-86126-697-9.
Wikimedia Commons has media related to Lockheed YF-12.
Retrieved from "https://en.wikipedia.org/w/index.php?title=Lockheed_YF-12&oldid=859559940"