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The '''] XF-88 Voodoo''' was a long-range, twin-engine ] ] designed for the ]. Although it never entered service, its design was adapted for the subsequent ]. The '''] XF-88 Voodoo''' was a long-range, twin-engine ] ] designed for the ].{{Citation needed|date=May 2011}}
Although it never entered service, its design was adapted for the subsequent ].{{Citation needed|date=May 2011}}



==Design and development== ==Design and development==
The XF-88 originated from a ] ] requirement for a long-range 'penetration fighter' to escort ]s to their targets. It was to be essentially a jet-powered replacement for the wartime ] that had escorted ] bombers over ]. It was to have a combat radius of 900 mi (1,450 km) and high performance. McDonnell began work on the aircraft, dubbed '''Model 36''', on 1 April 1946. On 20 June the company was given a contract for two prototypes designated '''XP-88'''. ] was Chief of Aerodynamics on this project. The XF-88 originated from a ] ] requirement for a long-range 'penetration fighter' to escort ]s to their targets.{{Citation needed|date=May 2011}} It was to be essentially a jet-powered replacement for the wartime ] that had escorted ] bombers over ].{{Citation needed|date=May 2011}} It was to have a combat radius of 900 mi (1,450 km) and high performance.{{Citation needed|date=May 2011}} McDonnell began work on the aircraft, dubbed '''Model 36''', on 1 April 1946.{{Citation needed|date=May 2011}} On 20 June the company was given a contract for two prototypes designated '''XP-88'''.{{Citation needed|date=May 2011}} ] was Chief of Aerodynamics on this project.{{Citation needed|date=May 2011}}


] ]
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] ]


The initial design was intended to have a ], but ] tests indicated aerodynamic problems that led to an extensive redesign. The USAAF (which became the ] on 17 September 1947) approved the changes. When the USAF altered its designation scheme in 1948, the still unflown prototypes were redesignated '''XF-88'''. It was dubbed '''Voodoo'''. The initial design was intended to have a ], but ] tests indicated aerodynamic problems that led to an extensive redesign.{{Citation needed|date=May 2011}} The USAAF (which became the ] on 17 September 1947) approved the changes.{{Citation needed|date=May 2011}} When the USAF altered its designation scheme in 1948, the still unflown prototypes were redesignated '''XF-88'''.{{Citation needed|date=May 2011}} It was dubbed '''Voodoo'''.{{Citation needed|date=May 2011}}

The Voodoo had a low/mid-mounted wing, ] to 35°.{{Citation needed|date=May 2011}} The two engines were in the lower fuselage, with jetpipes beneath the rear fuselage.{{Citation needed|date=May 2011}} The prototypes carried XJ34 engines, although the production '''F-88A''' would have had two ] turbojets with 5,920 lbf (26.33 kN) each.{{Citation needed|date=May 2011}} Intakes were mounted in the wing roots.{{Citation needed|date=May 2011}} The Voodoo's short nose had no radar, being intended to house an armament of six 20 mm (.79 in) ].{{Citation needed|date=May 2011}}


The first XF-88 made its maiden flight on 20 October 1948.<ref name="Knaackp317"> Knaack 1978, p.317.</ref> It had non-afterburning engines and no armament.{{Citation needed|date=May 2011}} It proved to be underpowered, leading to the decision to install afterburners on the second prototype, which was designated '''XF-88A''' and made its first flight on 26 April 1949 (The first prototype was modified to the same standard).{{Citation needed|date=May 2011}}
The Voodoo had a low/mid-mounted wing, ] to 35°. The two engines were in the lower fuselage, with jetpipes beneath the rear fuselage. The prototypes carried XJ34 engines, although the production '''F-88A''' would have had two ] turbojets with 5,920&nbsp;lbf (26.33&nbsp;kN) each. Intakes were mounted in the wing roots. The Voodoo's short nose had no radar, being intended to house an armament of six 20&nbsp;mm (.79&nbsp;in) ].


The first XF-88 made its maiden flight on 20 October 1948.<ref name="Knaackp317"> Knaack 1978, p.317.</ref> It had non-afterburning engines and no armament. It proved to be underpowered, leading to the decision to install afterburners on the second prototype, which was designated '''XF-88A''' and made its first flight on 26 April 1949. (The first prototype was modified to the same standard.)


In a subsequent paper competition against the ] and ], the Voodoo lost to the XF-93, but the decision on production was later delayed until a 'fly-off' competition could be held. In that fly-off, held in the summer of ], the XF-88 proved the winner, but changes in Air Force requirements led the penetration fighter to be cancelled entirely. In a subsequent paper competition against the ] and ], the Voodoo lost to the XF-93, but the decision on production was later delayed until a 'fly-off' competition could be held.{{Citation needed|date=May 2011}} In that fly-off, held in the summer of ], the XF-88 proved the winner, but changes in Air Force requirements led the penetration fighter to be cancelled entirely.{{Citation needed|date=May 2011}}


McDonnell proposed a naval version of the XF-88, a two-seat operational trainer, and a ] variant, but none were built. The first prototype was modified to '''XF-88B''' standard, with a nose-mounted ] ] engine added to the two existing turbojets. This was used for flight testing through ], and achieved speeds slightly exceeding ],<ref>{{cite web|url=http://www.hq.nasa.gov/office/pao/History/SP-445/ch4-8.htm|title=NASA History pages|accessdate=2007-09-04}}</ref> the first propeller-equipped aircraft to do so. Both prototypes were scrapped by ]. McDonnell proposed a naval version of the XF-88, a two-seat operational trainer, and a ] variant, but none were built.{{Citation needed|date=May 2011}} The first prototype was modified to '''XF-88B''' standard, with a nose-mounted ] ] engine added to the two existing turbojets.{{Citation needed|date=May 2011}} This was used for flight testing through ], and achieved speeds slightly exceeding ],<ref>{{cite web|url=http://www.hq.nasa.gov/office/pao/History/SP-445/ch4-8.htm|title=NASA History pages|accessdate=2007-09-04}}</ref> the first propeller-equipped aircraft to do so. Both prototypes were scrapped by ].{{Citation needed|date=May 2011}}


A considerably enlarged version of the basic design was developed following the cancellation of the XF-88, becoming the ], the first production version of which flew on 29 September 1954. The basic layout of two engines under the tail would also appear in the redesign of an upgraded F3H Demon which would see service as the very successful ]. A considerably enlarged version of the basic design was developed following the cancellation of the XF-88, becoming the ], the first production version of which flew on 29 September 1954.{{Citation needed|date=May 2011}} The basic layout of two engines under the tail would also appear in the redesign of an upgraded F3H Demon which would see service as the very successful ].{{Citation needed|date=May 2011}}


==Operators== ==Operators==

Revision as of 20:56, 7 May 2011

XF-88 Voodoo
Role Escort fighterType of aircraft
Manufacturer McDonnell
First flight 20 October 1948
Status Cancelled
Primary user United States Air Force
Number built 2
Developed into F-101 Voodoo

The McDonnell XF-88 Voodoo was a long-range, twin-engine jet fighter aircraft designed for the United States Air Force.

Although it never entered service, its design was adapted for the subsequent F-101 Voodoo.


Design and development

The XF-88 originated from a 1946 United States Army Air Forces requirement for a long-range 'penetration fighter' to escort bombers to their targets. It was to be essentially a jet-powered replacement for the wartime P-51 Mustang that had escorted B-17 Flying Fortress bombers over Germany. It was to have a combat radius of 900 mi (1,450 km) and high performance. McDonnell began work on the aircraft, dubbed Model 36, on 1 April 1946. On 20 June the company was given a contract for two prototypes designated XP-88. Dave Lewis was Chief of Aerodynamics on this project.

The engineering team stands after Flight 100.
File:Xf-88B.jpg
Supersonic jet-turboprop hybrid XF-88B
Landing the XF-88

The initial design was intended to have a V-shaped tail, but wind tunnel tests indicated aerodynamic problems that led to an extensive redesign. The USAAF (which became the United States Air Force on 17 September 1947) approved the changes. When the USAF altered its designation scheme in 1948, the still unflown prototypes were redesignated XF-88. It was dubbed Voodoo.

The Voodoo had a low/mid-mounted wing, swept to 35°. The two engines were in the lower fuselage, with jetpipes beneath the rear fuselage. The prototypes carried XJ34 engines, although the production F-88A would have had two Westinghouse J46 turbojets with 5,920 lbf (26.33 kN) each. Intakes were mounted in the wing roots. The Voodoo's short nose had no radar, being intended to house an armament of six 20 mm (.79 in) M39 cannon.

The first XF-88 made its maiden flight on 20 October 1948. It had non-afterburning engines and no armament. It proved to be underpowered, leading to the decision to install afterburners on the second prototype, which was designated XF-88A and made its first flight on 26 April 1949 (The first prototype was modified to the same standard).


In a subsequent paper competition against the Lockheed XF-90 and North American YF-93, the Voodoo lost to the XF-93, but the decision on production was later delayed until a 'fly-off' competition could be held. In that fly-off, held in the summer of 1950, the XF-88 proved the winner, but changes in Air Force requirements led the penetration fighter to be cancelled entirely.

McDonnell proposed a naval version of the XF-88, a two-seat operational trainer, and a reconnaissance variant, but none were built. The first prototype was modified to XF-88B standard, with a nose-mounted Allison T38 turboprop engine added to the two existing turbojets. This was used for flight testing through 1956, and achieved speeds slightly exceeding Mach 1.0, the first propeller-equipped aircraft to do so. Both prototypes were scrapped by 1958.

A considerably enlarged version of the basic design was developed following the cancellation of the XF-88, becoming the F-101 Voodoo, the first production version of which flew on 29 September 1954. The basic layout of two engines under the tail would also appear in the redesign of an upgraded F3H Demon which would see service as the very successful F-4 Phantom II.

Operators

 United States

Variants

XF-88A
XF-88B

Specifications (XF-88A)

General characteristics

  • Crew: one

Performance

Armament

See also

Related development

Aircraft of comparable role, configuration, and era

References

Notes

  1. Knaack 1978, p.317.
  2. "NASA History pages". Retrieved 2007-09-04.

Bibliography

  • Dorr, Robert F. and Donald, David. Fighters of the United States Air Force. London: Temple, 1990. ISBN 0 600 55094 X,
  • Knaack, Marcelle Size. Encyclopedia of US Air Force Aircraft and Missile Systems: Volume 1 Post-World War II Fighters, 1945-1973.. Washington: Office of Air Force History, 1978. ISBN 0-912799-19-6.

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