Vought F-8 Crusader

F-8 (F8U) Crusader
An F-8E from VMF(AW)-212 in 1965
Role	Fighter aircraft
National origin	United States
Manufacturer	Vought
First flight	25 March 1955
Introduction	March 1957
Retired	1976 (fighter, U.S. Navy) 29 March 1987 (photo reconnaissance, U.S. Naval Reserve) 1991 (Philippines) 19 December 1999 (fighter, France)
Status	Retired completely in 2000
Primary users	United States Navy United States Marine Corps French Navy Philippine Air Force
Number built	1,219[1]
Developed into	Vought XF8U-3 Crusader III LTV A-7 Corsair II

The Vought F-8 Crusader (originally F8U) was a single-engine, supersonic, carrier-based air superiority jet aircraft^[2] built by Vought for the United States Navy and Marine Corps, replacing the Vought F7U Cutlass, and for the French Navy. The first F-8 prototype was ready for flight in February 1955. The F-8 served principally in the Vietnam War. The Crusader was the last American fighter with guns as the primary weapon, earning it the title "The Last of the Gunfighters".^[3]

The RF-8 Crusader was a photo-reconnaissance development and operated longer in U.S. service than any of the fighter versions. RF-8s played a crucial role in the Cuban Missile Crisis, providing essential low-level photographs impossible to acquire by other means.^[3] U.S. Naval Reserve units continued to operate the RF-8 until 1987.

Design and development

In September 1952, the United States Navy announced a requirement for a new fighter. It was to have a top speed of Mach 1.2 at 30,000 ft (9,144.0 m) with a climb rate of 25,000 ft/min (127.0 m/s), and a landing speed of no more than 100 mph (160 km/h).^[4] Korean War experience had demonstrated that 0.50 inch (12.7 mm) machine guns were no longer sufficient and as the result the new fighter was to carry a 20 mm (0.79 in) cannon. In response, the Vought team led by John Russell Clark, created the V-383. Unusual for a fighter, the aircraft had a high-mounted wing which necessitated the use of a fuselage-mounted short and light landing gear.

The Crusader was powered by a Pratt and Whitney J57 turbojet engine. The engine was equipped with an afterburner, that, unlike on later engines, was either fully lit, or off (i.e. it did not have "zones"). The engine produced 18,000 lb of thrust at full power, enough to allow the F-8 to climb straight up in clean configuration. The Crusader was the first jet fighter in US service to reach 1,000 mph; US Navy pilot R.W. Windsor reached 1,015 mph on a flight in 1956.^[5]

The most innovative aspect of the design was the variable-incidence wing which pivoted by 7° out of the fuselage on takeoff and landing (not to be confused with variable-sweep wing). This afforded increased lift due to a greater angle of attack without compromising forward visibility because the fuselage stayed level.^[3][4] This innovation is credited as the most important factor that led to the F-8's development team being awarded the Collier Trophy in 1956.^[6] Simultaneously, the lift was augmented by leading-edge slats drooping by 25° and inboard flaps extending to 30°. The rest of the aircraft took advantage of contemporary aerodynamic innovations with area ruled fuselage, all-moving stabilators, dog-tooth notching at the wing folds for improved yaw stability, and liberal use of titanium in the airframe. Power came from the Pratt & Whitney J57 afterburning turbojet. The armament, as specified by the Navy, consisted primarily of four 20 mm (.79 in) autocannon; the Crusader happened to be the last U.S. fighter designed with guns as its primary weapon.^[3] They were supplemented with a retractable tray with 32 unguided Mk 4/Mk 40 Folding-Fin Aerial Rocket (Mighty Mouse FFARs), and cheek pylons for two guided AIM-9 Sidewinder air-to-air missiles.^[4] Vought also presented a tactical reconnaissance version of the aircraft called the V-392.

Major competition came from the Grumman F-11 Tiger, the upgraded twin-engine McDonnell F3H Demon (which would eventually become the McDonnell Douglas F-4 Phantom II), and lastly, the North American F-100 Super Sabre hastily adapted to carrier use and dubbed the "Super Fury".

In May 1953, the Vought design was declared a winner and in June, Vought received an order for three XF8U-1 prototypes (after adoption of the unified designation system in September 1962, the F8U became the F-8). The first prototype flew on 25 March 1955 with John Konrad at the controls. The aircraft exceeded the speed of sound during its maiden flight.^[3] The development was so trouble-free that the second prototype, along with the first production F8U-1, flew on the same day, 30 September 1955. On 4 April 1956, the F8U-1 performed its first catapult launch from Forrestal.

Crusader III

In parallel with the F8U-1s and -2s, the Crusader design team was also working on a larger aircraft with ever greater performance, internally designated as the V-401. Although the Vought XF8U-3 Crusader III was externally similar to the Crusader and sharing with it such design elements as the variable incidence wing, the new fighter was significantly larger and shared few components.

Operational history

Prototype XF8U-1s were evaluated by VX-3 beginning in late 1956, with few problems noted. Weapons development was conducted at Naval Air Weapons Station China Lake and a China Lake F8U-1 set a U.S. National speed record in August 1956. Commander "Duke" Windsor set, broke, and set a new Level Flight Speed Record of 1,015.428 mph (1,634.173 km/h) on 21 August 1956 beating the previous record of 822 mph (1,323 km/h) set by a USAF F-100, however, the world speed record of 1,132 mph (1,822 km/h), set by the British Fairey Delta 2, on 10 March 1956, was not broken.^[7]

An early F8U-1 was modified as a photo-reconnaissance aircraft, becoming the first F8U-1P, subsequently the RF-8A equipped with cameras rather than guns and missiles. On 16 July 1957, Major John H. Glenn, JR, USMC, completed the first supersonic transcontinental flight in a F8U-1P, flying from NAS Los Alamitos, California to Floyd Bennett Field, New York in 3 hours, 23 minutes and 8.3 seconds.^[8]

First fleet operators

Air Development Squadron Three was established in November 1948 and tasked with evaluating new and existing naval aircraft, equipment and methods and also developing tactics and procedures for these.

VX-3 was one of the first units to receive the F8U-1 in December 1956, and was the first to operate the type in April 1957, from the USS Franklin D. Roosevelt. VX-3 was the first unit to qualify for carrier operations but several aircraft were lost in accidents, in several cases killing their pilots.

The first fleet squadron to fly the Crusader was VF-32 at NAS Cecil Field, Florida, in 1957, deploying to the Mediterranean late that year on Saratoga. VF-32 renamed the squadron the "Swordsmen" in keeping with the Crusader theme. The Pacific Fleet received the first Crusaders at NAS Moffett Field in Northern California and the VF-154 "Grandslammers" (named in honor of the new 1,000 mph jets and subsequently renamed the "Black Knights") began their F-8 operations. Later in 1957, in San Diego VMF-122 accepted the first Marine Corps Crusaders.

In 1962, the Defense Department standardized military aircraft designations generally along Air Force lines. Consequently, the F8U became the F-8, with the original F8U-1 redesignated F-8A.

Fleet service

The Crusader became a "day fighter" operating off the aircraft carriers. At the time, U.S. Navy carrier air wings had gone through a series of day and night fighter aircraft due to rapid advances in engines and avionics. Some squadrons operated aircraft for very short periods before being equipped with a newer higher performance aircraft. The Crusader was the first post-Korean War aircraft to have a relatively long tenure with the fleet and like the USAF Republic F-105 Thunderchief, a contemporary design, might have stayed in service longer if not for the Vietnam war and resulting attrition from combat and operational losses.

Cuban Missile Crisis

The unarmed Crusader was operated aboard carriers as a detachment (Det) from either VFP-62 or VFP-63 to provide photo reconnaissance capability as RF-8A proved ideal for the task of getting low altitude detailed photographs.^[9] During the Cuban Missile Crisis in 1962, RF-8As flew extremely hazardous low-level photo reconnaissance missions over Cuba with overflights beginning on 23 October 1962. These were the first true operational flights of the F-8 Crusader. Flights of RF-8As, operating in several pairs of aircraft, with each pair assigned a different target, left Key West twice each day, to fly over Cuba at low level, then return to Jacksonville, where the film was offloaded and developed, to be rushed north to the Pentagon.^[10]

These flights confirmed that the Soviet Union was setting up IRBMs in Cuba. The RF-8As also monitored the withdrawal of the Soviet missiles. To keep score after an overflight, each aircraft was given a stencil of a dead chicken. The overflights went on for about six weeks and returned a total of 160,000 images. The pilots who flew the missions all received Distinguished Flying Crosses, while VFP-62 received the prestigious U.S. Navy Unit Commendation.^[11]

Mishap rate

The Crusader was not an easy aircraft to fly, and was often unforgiving in carrier landings, where it suffered from yaw instability, and the poorly designed, castoring nose undercarriage made steering on the deck problematic. Safe landings required the carriers to steam at full speed to lower the relative landing speed for Crusader pilots. The stacks of the oil-burning carriers on which the Crusader served belched thick black smoke, sometimes obscuring the flight deck, leaving the Crusader's pilot dependent on the landing signal officer's radioed instructions.^[6] It earned a reputation as an "ensign killer" during its early service introduction.^[12] The nozzle and air intake were so low when the aircraft was on the ground or the flight deck that the crews called the aircraft "the Gator". Not surprisingly, the Crusader's mishap rate was relatively high compared to its contemporaries, the Douglas A-4 Skyhawk and the F-4 Phantom II. However, the aircraft did possess some amazing capabilities, as proved when several Crusader pilots took off with the wings folded. One of these episodes took place on 23 August 1960; a Crusader with the wings folded took off from Napoli Capodichino in full afterburner, climbed to 5,000 ft (1,500 m) and then returned to land successfully. The pilot, absent minded but evidently a good "stick man," complained that the control forces were higher than normal. The Crusader was capable of flying in this state, though the pilot would be required to reduce aircraft weight by ejecting stores and fuel prior to landing.^[3] In all, 1,261 Crusaders were built. By the time it was withdrawn from the fleet, 1,106 had been involved in mishaps.^[13] Only a handful of them were lost to enemy fire in Vietnam.^[13]

Vietnam War

When conflict erupted in the skies over North Vietnam, it was U.S. Navy Crusaders from the USS Hancock that first tangled with Vietnam People's Air Force (North Vietnamese Air Force) MiG-17s, on 3 April 1965.^[14] The MiGs claimed the downing of a Crusader, and Lt Pham Ngoc Lan's gun camera revealed that his cannons had set an F-8 ablaze, but Lieutenant Commander Spence Thomas had managed to land his damaged Crusader at Da Nang,^[15][16] the remaining F-8s returning safely to their carrier. At the time, the Crusader was the best dogfighter the United States had against the nimble North Vietnamese MiGs. The U.S. Navy had evolved its "night fighter" role in the air wing to an all-weather interceptor, the F-4 Phantom II, equipped to engage incoming bombers at long range with missiles such as AIM-7 Sparrow as their sole air-to-air weapons, and maneuverability was not emphasized in their design. Some experts believed that the era of the dogfight was over as air-to-air missiles would knock down adversaries well before they could get close enough to engage in dogfighting. As aerial combat ensued over North Vietnam from 1965 to 1968, it became apparent that the dogfight was not over and the F-8 Crusader and a community trained to prevail in air-to-air combat was a key ingredient to success.

The Crusader also became a "bomb truck" in war, with both ship-based U.S. Navy units and land-based U.S. Marine Corps squadrons attacking communist forces in both North and South Vietnam.^[12]

USMC Crusaders flew only in the south, while U.S. Navy Crusaders flew only from the small Essex-class carriers. Marine Crusaders also operated in close air support missions.

Despite the "last gunfighter" moniker, the F-8s achieved only four victories with their cannon; the remainder were accomplished with AIM-9 Sidewinder missiles,^[17] partly due to the propensity of the 20 mm (.79 in) Colt Mk 12 cannons' feeding mechanism to jam under G-loading during high-speed dogfighting maneuvers.^[18] Between June and July 1966, during 12 engagements over North Vietnam, Crusaders claim four MiG-17s for two losses.^[19] The Crusader would claim the best kill ratio of any American type in the Vietnam War, 19:3.^[3] Of the 19 aircraft claimed during aerial combat, 16 were MiG-17s and three were MiG-21s.^[17] U.S. records only indicate 3 F-8s lost in aerial combat, all to MiG-17 cannon fire in 1966, but the NVAF claimed 11 F-8s were shot down by MiGs.^[20][21][22] A total of 170 F-8 Crusaders would be lost to all causes during the war.^[23]

F-8 pilots credited with shooting down North Vietnamese aircraft^[12]

Name	Squadron	Aircraft	Date
CDR Harold L. Marr	VF-211	MiG-17	12 June 1966
LT Eugene J. Chancy	VF-211	MiG-17	21 June 1966
LTJG Philip V. Vampatella	VF-211	MiG-17	21 June 1966
CDR Richard M. Bellinger	VF-162	MiG-21	9 October 1966
CDR Marshall O. Wright	VF-211	MiG-17	1 May 1967
CDR Paul H. Speer	VF-211	MiG-17	19 May 1967
LTJG Joseph M. Shea	VF-211	MiG-17	19 May 1967
LCDR Bobby C. Lee	VF-24	MiG-17	19 May 1967
LT Phillip R. Wood	VF-24	MiG-17	19 May 1967
LCDR Marion H. Isaacks	VF-24	MiG-17	21 July 1967
LCDR Robert L. Kirkwood	VF-24	MiG-17	21 July 1967
LCDR Ray G. Hubbard, Jr.	VF-211	MiG-17	21 July 1967
LT Richard E. Wyman	VF-162	MiG-17	14 December 1967
CDR Lowell R. Myers	VF-51	MiG-21	26 June 1968
LCDR John B. Nichols	VF-191	MiG-17	9 July 1968
CDR Guy Cane	VF-53	MiG-17	29 July 1968
LT Norman K. McCoy, Jr.	VF-51	MiG-21	1 August 1968
LT Anthony J. Nargi	VF-111	MiG-21	19 September 1968
LT Gerald D. Tucker	VF-211	MiG-17	22 April 1972

Twilight service with U.S. Navy

LTV built and delivered the 1,219th (and last) U.S. Navy Crusader to VF-124 at NAS Miramar on 3 September 1964.^[1]

The last active duty Navy Crusader fighter variants were retired from VF-191 and VF-194 aboard Oriskany in 1976 after almost two decades of service, setting a first for a Navy fighter.

The photo reconnaissance variant continued to serve in the active duty Navy for yet another 11 years, with VFP-63 flying RF-8Gs up to 1982, and with the Naval Reserve flying their RF-8Gs in two squadrons (VFP-206 and VFP-306) at Naval Air Facility Washington / Andrews AFB until the disestablishment of VFP-306 in 1984 and VFP-206 on 29 March 1987 when the last operational Crusader was turned over to the National Air and Space Museum.^[24]

The F-8 Crusader is the only aircraft to have used the AIM-9C which is a radar-guided variant of the Sidewinder. When the Crusader retired, these missiles were converted to the AGM-122 Sidearm anti-radiation missiles used by United States attack helicopters to knock out enemy radars.

NASA

Several modified F-8s were used by NASA in the early 1970s, proving the viability of both digital fly-by-wire and supercritical wings.

French Navy

When the French Navy's air arm, the Aéronavale, required a carrier based fighter in the early 1960s to serve aboard the new carriers Clemenceau and Foch, the F-4 Phantom, then entering service with the United States Navy, proved to be too large for the small French ships. Following carrier trials aboard Clemenceau on 16 March 1962, by two VF-32 F-8s from the American carrier Saratoga, the Crusader was chosen and 42 F-8E(FN)s were ordered, the last Crusaders produced.

The French Crusaders were based on the F-8E, but were modified in order to allow operations from the small French carriers, with the maximum angle of incidence of the aircraft's wing increased from five to seven degrees and blown flaps fitted. The aircraft's weapon system was modified to carry two French Matra R.530 radar or infra-red missiles as an alternative to Sidewinders, although the ability to carry the American missile was retained.^[25] Deliveries started in October 1964 and continued until February 1965, with the Aéronavale's first squadron, Flotille 12F reactivated on 1 October 1964.^[25] To replace the old Corsairs, Flotille 14.F received its Crusaders on 1 March 1965.^[26][27]

In October 1974, (on Clemenceau) and June 1977 (on Foch), Crusaders from 14.F squadron participated in the Saphir missions over Djibouti. On 7 May 1977, two Crusaders went separately on patrol against supposedly French Air Force (4/11 Jura squadron) F-100 Super Sabres stationed at Djibouti. The leader intercepted two fighters and engaged a dogfight (supposed to be a training exercise) but quickly called his wingman for help as he had actually engaged two Yemeni Mikoyan-Gurevich MiG-21s. The two French fighters switched their master armament to "on" but, ultimately, everyone returned to their bases. This was the only combat interception by French Crusaders.

The Aéronavale Crusaders flew combat missions over Lebanon in 1983 escorting Dassault-Breguet Super Étendard strike aircraft. In October 1984, France sent Foch for Operation Mirmillon off the coast of Libya, intended to calm Colonel Ghaddafi down, with 12.F squadron. The escalation of the situation in the Persian Gulf, due to the Iran-Iraq conflict, triggered the deployment of Clemenceau task force and its air wing, including 12.F squadron. 1993 saw the beginning of the missions over ex-Yugoslavia. Crusaders were launched from both carriers cruising in the Adriatic Sea. These missions ceased in June 1999 with Operation Trident over Kosovo.

The French Crusaders were subject to a series of modifications throughout their life, being fitted with new F-8J-type wings in 1969 and having modified afterburners fitted in 1979.^[28] Armament was enhanced by the addition of R550 Magic infra-red guided missiles in 1973, with the improved, all-aspect Magic 2 fitted from 1988. The obsolete R.530 was withdrawn from use in 1989, leaving the Crusaders without a radar-guided missile.^[29] In 1989, when it was realised that the Crusader would not be replaced for several years, it was decided to refurbish the Crusaders to extend their operating life. Each aircraft was rewired and had its hydraulic system refurbished, while the airframe was strengthened to extend fatigue life. Avionics were improved, with a modified navigation suite and a new radar-warning receiver.^[30][31] The 17 refurbished aircraft were redesignated as F-8P (P used for "Prolongé" -extended- and not to be confused with the Philippine F-8P).^[32] Although the French Navy participated in combat operations in 1991 during Operation Desert Storm and over Kosovo in 1999, the Crusaders stayed behind and were eventually replaced by the Rafale M in 2000 as the last of the breed in military service.

Philippine Air Force

In late 1977, the Philippine government purchased 35 secondhand U.S. Navy F-8Hs that were stored at Davis-Monthan AFB in Arizona.^[33] Twenty-five of them were refurbished by Vought and the remaining 10 were used for spare parts.^[33] As part of the deal, the U.S. would train Philippine pilots in using the TF-8A.^[33] They were mostly used for intercepting Soviet bombers.^[33] The F-8s were grounded in 1988 and were finally withdrawn from service in 1991 after they were badly damaged by the Mount Pinatubo eruption, and have since been offered for sale as scrap.

Variants

• XF8U-1 (XF-8A) (V-383) – the two original unarmed prototypes.
• F8U-1 (F-8A) – first production version, J57-P-12 engine replaced with more powerful J57-P-4A starting with 31st production aircraft, 318 built.
• YF8U-1 (YF-8A) – one F8U-1 fighter used for development testing.
• YF8U-1E (YF-8B) – one F8U-1 converted to serve as an F8U-1E prototype.
• F8U-1E (F-8B) – added a limited all-weather capability thanks to the AN/APS-67 radar, the unguided rocket tray was sealed shut because it was never used operationally, first flight: 3 September 1958, 130 built.
• XF8U-1T – one XF8U-2NE used for evaluation as a two-seat trainer.
• F8U-1T (TF-8A) (V-408) – two-seat trainer version based on F8U-2NE, fuselage stretched 2 ft (0.61 m), internal armament reduced to two cannon, J57-P-20 engine, first flight 6 February 1962. The Royal Navy was initially interested in the Rolls-Royce Spey-powered version of TF-8A but chose the Phantom II instead. Only one TF-8A was built, although several retired F-8As were converted to similar two-seat trainers.
• YF8U-2 (YF-8C) – two F8U-1s used for flight testing the J57-P-16 turbojet engine.
• F8U-2 (F-8C) – J57-P-16 engine with 16,900 lbf (75 kN) of afterburning thrust, ventral fins added under the rear fuselage in an attempt to rectify yaw instability, Y-shaped cheek pylons allowing two Sidewinder missiles on each side of the fuselage, AN/APQ-83 radar retrofitted during later upgrades. First flight: 20 August 1957, 187 built. This variant was sometimes referred to as Crusader II.^[34]
• F8U-2N (F-8D) – all-weather version, unguided rocket pack replaced with an additional fuel tank, J57-P-20 engine with 18,000 lbf (80 kN) of afterburning thrust, landing system which automatically maintained present airspeed during approach, incorporation of AN/APQ-83 radar. First flight: 16 February 1960, 152 built.
• YF8U-2N (YF-8D) – one aircraft used in the development of the F8U-2N.
• YF8U-2NE – one F8U-1 converted to serve as an F8U-2NE prototype.
• F8U-2NE (F-8E) – J57-P-20A engine, AN/APQ-94 radar in a larger nose cone, dorsal hump between the wings containing electronics for the AGM-12 Bullpup missile, payload increased to 5,000 lb (2,270 kg), Martin-Baker ejection seat, AN/APQ-94 radar replaced AN/APQ-83 radar in earlier F-8D. IRST sensor blister (round ball) was added in front of the canopy.^[35] First flight: 30 June 1961, 286 built.
• F-8E(FN) – air superiority fighter version for the French Navy, significantly increased wing lift due to greater slat and flap deflection and the addition of a boundary layer control system, enlarged stabilators, incorporated AN/APQ-104 radar, an upgraded version of AN/APQ-94. A total of 42 built.
• F-8H – upgraded F-8D with strengthened airframe and landing gear, with AN/APQ-84 radar. A total of 89 rebuilt.
• F-8J – upgraded F-8E, similar to F-8D but with wing modifications and BLC like on F-8E(FN), "wet" pylons for external fuel tanks, J57-P-20A engine, with AN/APQ-124 radar. A total of 136 rebuilt.
• F-8K – upgraded F-8C with Bullpup capability and J57-P-20A engines, with AN/APQ-125 radar. A total of 87 rebuilt.
• F-8L – F-8B upgraded with underwing hardpoints, with AN/APQ-149 radar. A total of 61 rebuilt.
• F-8P – 17 F-8E(FN) of the Aéronavale underwent a significant overhaul at the end of the 1980s to stretch their service life another 10 years. They were retired in 1999.^[36]
• F8U-1D (DF-8A) – several retired F-8A modified to controller aircraft for testing of the SSM-N-8 Regulus cruise missile. DF-8A was also modified as drone (F-9 Cougar) control which were used extensively by VC-8, NS Roosevelt Rds, PR; Atlantic Fleet Missile Range.
• DF-8F – retired F-8A modified as controller aircraft for testing of missiles including at the USN facility at China Lake.
• F8U-1KU (QF-8A) – retired F-8A modified into remote-controlled target drones
• YF8U-1P (YRF-8A) – prototypes used in the development of the F8U-1P photo-reconnaissance aircraft - V-392.
• F8U-1P (RF-8A) – unarmed photo-reconnaissance version of F8U-1E, 144 built.
• RF-8G – modernized RF-8As.
• LTV V-100 – revised "low-cost" development based on the earlier F-8 variants, created in 1970 to compete against the F-4E Phantom II, Lockheed CL-1200 and F-5-21 in a tender for U.S. Military Assistance Program (MAP) funding. The unsuccessful design was ultimately only a "paper exercise."^[37]
• XF8U-3 Crusader III (V-401) – new design loosely based on the earlier F-8 variants, created to compete against the F-4 Phantom II; J75-P-5A engine with 29,500 lbf (131 kN) of afterburning thrust, first flight: 2 June 1958, attained Mach 2.39 in test flights, canceled after five aircraft were constructed because the Phantom II won the Navy contract.

Operators

 France

• French Navy (Aéronavale)

 Philippines

• Philippine Air Force

 United States

• United States Navy
• United States Marine Corps
• NASA

Aircraft on display

France

F-8E(FN)

• 151732 (French Navy Side Number 1) - Musee des Avions de Chasse, Beaune.^[38]
• 151750 (French Navy Side Number 19) - Musée des Ailes Anciennes, Toulouse.^[39]

F-8P

• 151733 (French Navy Side Number 3) - Lann Bihoue Airport, Le Meneguen.^[40]
• 151735 (French Navy Side Number 4) - Musee Europeen de lAviation de Chasse, Montelimar-Ancone.^[41]
• 151738 (French Navy Side Number 7) - Aeronavale Base, Landivisau.^[42]
• 151741 (French Navy Side Number 10) - Musee de l air et de l Espace, (The Air and Space Museum), Paris, France.^[43]
• 151754 (French Navy Side Number 23) - Aeronavale Base, Landivisau.^[44]
• 151760 (French Navy Side Number 29) - Aeronavale Base, Landivisau.^[45]
• 151767 (French Navy Side Number 36) - Musee des Avions de Chasse, Beaune.^[46]
• 151768 (French Navy Side Number 37) - Airport in Cuers.^[47]
• 151770 (French Navy Side Number 39) - Aeronavale Base, Landivisau.^[48]

Philippines

F-8H

• 147056 - Philippine Air Force Aerospace Museum, Villamor AB, Manila.^[49]
• 148661 - Clark AB, Angeles.^[50]

United States

XF8U-1 (XF-8A)

• 138899 - Museum of Flight in Seattle, Washington.^[51]

XF8U-2 (XF-8B)

• 140448 - McAuliffe-Shepard Discovery Center in Concord, New Hampshire.^[52]

F8U-1 (F-8A)

• 141351 - NAS Jacksonville Heritage Park, Naval Air Station Jacksonville, Florida (relocated from former NAS Cecil Field).^[53]
• 141353 - Edwards AFB, California.^[54]
• 143703 - USS Hornet Museum, former Naval Air Station Alameda, Alameda, California.^[55]
• 143755 - Marine Corps Air Station Miramar, California.^[56]
• 143806 - Wings of Freedom Aviation Museum, former Naval Air Station Willow Grove, Willow Grove, Pennsylvania.^[57]
• 144427 - Pima Air and Space Museum adjacent to Davis-Monthan AFB in Tucson, Arizona.^[58]
• 145336 - Planes of Fame at Chino, California.^[59]
• 145347 - National Naval Aviation Museum at Naval Air Station Pensacola, Florida.^[60]
• 145349 - Pueblo Weisbrod Aircraft Museum, Pueblo, Colorado.^[61]
• 145397 - Naval Air Engineering Station Lakehurst, Lakehurst, New Jersey.^[62]

F8U-2 (F-8C)

• 145546 - Edwards AFB, California.^[63]
• 146963 - Marine Corps Air Station Beaufort, South Carolina.^[64]
• 146973 - Marine Corps Air Station Kaneohe Bay, Hawaii^[65]
• 147034 - (nose section only) USS Hornet Museum, former NAS Alameda, Alameda, California.^[66]
• 149150 - NAS Oceana Aviation Heritage Park, Naval Air Station Oceana, Virginia.^[67]

F8U-2N (F-8D)

• 148693 - Mid America Air Museum in Liberal, Kansas.^[68]

F8U-1P (RF-8G)

• 144617 - Flying Leatherneck Aviation Museum at Marine Corps Air Station Miramar, California^[69]
• 144618 - Celebrity Row, Davis-Monthan AFB (North Side), Tucson, Arizona.^[70]
• 145607 - Castle Air Museum (formerly Castle AFB), Atwater, California.^[71]
• 145608 - (nose section only) Pacific Coast Air Museum, Santa Rosa, California.^[72]
• 145609 - National Museum of Naval Aviation, Naval Air Station Pensacola, Pensacola, Florida.^[73]
• 145645 - USS Alabama Battleship Memorial Park, Mobile, Alabama.^[74]
• 146860 - Smithsonian Institution's National Air and Space Museum Udvar-Hazy Center in Chantilly, Virginia, adjacent to Dulles International Airport.^[75]

• 146882 - Frontiers of Flight Museum in Dallas, Texas.^[76]
• 146898 - Fort Worth Aviation Museum in Fort Worth, Texas.^[77]
• 150920 - Flying Leatherneck Aviation Museum at Marine Corps Air Station Miramar, California^[78]

F-8H

• 147909 - NAD Soroptimist Park, Kitsap Lake, Bremerton, Washington, about 1 mile away from Naval Hospital Bremerton. Aircraft is on loan from the National Naval Aviation Museum, Pensacola, Florida.^[79]

F-8J

• 150904 - Air Zoo in Kalamazoo, Michigan.^[80]

F8U-2 (F-8K)

• 145550 - USS Intrepid Museum in New York City, New York.^[81]
• 146931 - Estrella Warbirds Museum in Paso Robles, California.^[82]
• 146939 - Patriots Point Naval & Maritime Museum aboard ex-USS Yorktown (CV-10), Mount Pleasant, South Carolina.^[83]
• 146983 - Marine Corps Air Station Kaneohe Bay, Hawaii.^[84]
• 146985 - Valiant Air Command Warbird Museum at Space Coast Regional Airport in Titusville, Florida^[85]
• 146995 - Pacific Coast Air Museum, adjacent to the Sonoma County Airport in Santa Rosa, California^[86]
• 147030 - USS Midway Museum in San Diego, California.^[87]

F-8L

• 145449 - Naval Air Station Fallon, Fallon, Nevada.^[88]

Specifications (F-8E)

Data from The Great Book of Fighters^[89] and Quest for Performance^[90] Combat Aircraft since 1945^[91] Joseph F. Baugher ^[92]

General characteristics

• Crew: 1
• Payload: 5,000 lb (2,300 kg) of weapons
• Length: 54 ft 3 in (16.53 m)
• Wingspan: 35 ft 8 in (10.87 m)
• Height: 15 ft 9 in (4.80 m)
• Wing area: 375 ft² (34.8 m²)
• Airfoil: NACA 65A006 mod root, NACA 65A005 mod tip
• Aspect ratio: 3.42:1
• Empty weight: 17,541 lb (7,956 kg)
• Loaded weight: 29,000 lb (13,000 kg)
• Powerplant: 1 × Pratt & Whitney J57-P-20A afterburning turbojet
  • Dry thrust: 10,700 lbf (47.6 kN)
  • Thrust with afterburner: 18,000 lbf (80.1 kN)
• Zero-lift drag coefficient: 0.0133
• Drag area: 5.0 ft² (0.46 m²)
• Fuel capacity: 1,325 US gal (5,020 L)

Performance

• Maximum speed: Mach 1.86 (1,225 mph, 1,975 km/h) at 36,000 ft (11,000 m)
• Cruise speed: 570 mph (495 knots; 917 km/h)
• Combat radius: 450 mi (730 km)
• Ferry range: 1,735 mi (2,795 km) with external fuel
• Service ceiling: 58,000 ft (17,700 m)
• Rate of climb: 27,200 ft/min (162.3 m/s)
• Wing loading: 77.3 lb/ft² (377.6 kg/m²)
• Thrust/weight: 0.62
  
• Lift-to-drag ratio: 12.8

Armament

• Guns: 4× 20 mm (0.79 in) Colt Mk 12 cannons in lower fuselage, 125 rpg
• Hardpoints: 2× side fuselage mounted Y-pylons (for mounting AIM-9 Sidewinders and Zuni rockets) and 2× underwing pylon stations holding up to 4,000 lb (2,000 kg) of payload:
• Rockets:
  
  • 2× LAU-10 rocket pods (each with 4× 5 inch (127mm) Zuni rockets)
• Missiles:
  
  • Air-to-air missiles:
    • 4× AIM-9 Sidewinder or Matra Magic (mounted only on F-8E(FN) of French Navy)
  • Air-to-surface missiles:
    • 2× AGM-12 Bullpup
• Bombs:
  
  • 12× 250 lb (113 kg) Mark 81 bombs or
  • 8× 500 lb (227 kg) Mark 82 bombs or
  • 4× 1,000 lb (454 kg) Mark 83 bombs or
  • 2× 2,000 lb (907 kg) Mark 84 bombs

Avionics

• Magnavox AN/APQ-84 or AN/APQ-94 Fire-control radar

See also

Related development

• LTV A-7 Corsair II
• Vought XF8U-3 Crusader III
• Vought YA-7F

Aircraft of comparable role, configuration and era

• Grumman F-11 Tiger
• North American F-100 Super Sabre

Related lists

• List of fighter aircraft
• List of military aircraft of the United States

References

Notes

Bibliography

External links

Wikimedia Commons has media related to Vought F-8 Crusader.

• F-8 Crusader factsheet on GlobalSecurity.org
• "Aircraft Familiarization - F8U-2N (1961)" on YouTube
• (1968) NAVAIR 01-45HHB-1 NATOPS Flight Manual Navy Model F-8D, F-8E Aircraft
• (1978) NAVAIR 01-45HHB-1 NATOPS Flight Manual Navy Model RF-8G Aircraft

Aircraft produced by Vought / LTV Aerospace Fighters VE-7/VE-8/VE-9 V-141 V-143 FU XF2U XF3U F4U XF5U F6U F7U F8U/F-8/XF8U-3 Model 1600 Scout / Attack O2U O3U O4U O5U OS2U XSO2U SU SBU SB2U XSB3U TBU AU A2U A-7 YA-7F Experimental / Unbuilt XC-142 V-173 XS2U XWU Names Corsair O2U SBU F4U/AU A-7 (II) Others Crusader (I/II) Crusader III Cutlass Kingfisher Pirate Sea Wolf Vindicator

United States Navy fighter designations pre-1962 General Aviation Brewster FA FA2 F2A F3A Boeing FB F2B F3B F4B F5B F6B F7B F8B Curtiss CF F2C F3C F4C F5C1 F6C F7C F8C F9C F10C F11C F12C F13C F14C F15C Douglas McDonnell XFD F2D2 F3D F4D F5D F6D FD F2D to "H" Grumman FF F2F F3F F4F F5F F6F F7F F8F F9F-1 to -5 F9F-6 to -8 F10F F11F F12F Eberhart Goodyear FG F2G FG F2G Hall McDonnell FH FH F2H F3H F4H Berliner-Joyce North American FJ F2J F3J FJ-1 FJ-2/3 FJ-4 Loening Bell FL FL YF2L-1 F2L-1K F3L General Motors FM F2M F3M Naval Aircraft Factory FN Lockheed FO (I) FO (II) Ryan FR F2R F3R Supermarine FS Northrop FT F2T Vought FU F2U F3U F4U F5U F6U F7U F8U F8U-3 Lockheed FV Wright CC&F WP F2W F3W FW2 F2W2 F3W2 F4W Convair FY F2Y 1 Not assigned  • 2 Assigned to a different manufacturer's type See also: Aeromarine AS  • Vought VE-7

United States tri-service fighter aircraft designations post-1962 F-1C/F-1E F-2 F-3 F-4 F-5 F-6 F-7 F-8 F-9 F-10 F-11 YF-12 F-131 F-14 F-15/E F-16 YF-17 F/A-18/E/F F-191 F-20 F-21 YF-22/F-22 YF-23 F-24 to F-341 F-35 1 Not assigned See also: "F-19"  • F-117  • Pre-1962 list

United States military reconnaissance aircraft designations, Army/Air Force and Tri-Service systems Army/Air Force main sequence (1930-1962) Prefix F-, 1930–1947 F-1 F-2 F-3 F-4 F-5 F-6 F-7 F-8 F-9 F-10 F-11 F-12 F-13 F-14 F-15 Prefix R-, 1947–1962 R-11 R-12 R-16 Reconnaissance-strike sequence (1960-1962) RS-70 RS-71 Tri-service main sequence (1962-present) R-1 Reconnaissance subtypes Converted fighters RF-4 RF-8 RF-80 RF-101 RF-104 Converted bombers RB-17 RB-29 RB-47 RB-52 RB-66

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