SNCASO SO.8000 Narval

The French Navy ordered two prototype SO.8000 strike fighters on 31 May 1946 to equip its aircraft carriers. If the prototypes were successful, it planned to order five pre-production models and sixty-five production aircraft. Designer Jean Dupuy developed a twin-boom pusher configuration design with a crescent wing and tricycle landing gear. The horizontal stabilizer was connected at the tops of the vertical stabilizers at the ends of the booms to avoid turbulence from the contra-rotating propeller. The pilot was provided with an ejection seat and the aircraft was intended to be fitted with six {{convert|20|mm|adj=on|sp=us|1}} MG 151 autocannon in the nose and to be able to carry {{convert|1000|kg|lb|sp=us}} of ordnance under the wings. A radar system was planned to be fitted in the lower front portion of the booms while the fuel was stowed between the cockpit and the engine. Dupuy wanted to use a British Rolls-Royce Griffon engine, but it proved to be too difficult to obtain. He planned to substitute a Hispano-Suiza 12Z instead, but the engine was still too immature to be used and he had to settle for an Arsenal 12H (a copy of the Junkers Jumo 213) driving the contra-rotating propeller.Buttler, p. 84; Carbonel, p. 98 Ducts on the sides of the fuselage provided air for the engine radiator while the engine's air was provided by a prominent scoop on the left side of the fuselage.Pearce

Only the first prototype was intended to be fitted with the nose guns, so the second prototype was completed first, beginning taxiing tests in December 1948. Test pilot Jacques Guignard attempted to make the first flight on 13 January 1949, but he was unable to take off despite achieving a speed of {{convert|200|km/h|sp=us|0}}. Despite some modifications made to alleviate the problem, the second prototype still failed to take off on 25 January. The design team resorted to cutting V-shapes into the booms to give it an angle of 2°15' which would allow the aircraft to be trimmed nose-upwards to facilitate a takeoff. Further high-speed taxiing trials were made in February with promising results, but the elevator had to be enlarged from an area of {{cvt|1.75|to|2.6|sqm}}, extending it past the vertical stabilizers, before it could make its maiden flight on 1 April. After modifications to its spoiler, elevator and landing gear doors, the aircraft made its next flight on 21 April.Buttler, pp. 84–85

The Narval was exhibited in that year's Paris Air Show in May and resumed flight testing. On 24 May it reached a speed of {{cvt|500|km/h|0}} at which time it began pitching oscillations and the controls became harder to move. The aircraft's airframe and engine were modified in August and the engine's crankshaft broke during a flight on 7 September. The Chauvière propeller proved to be a disappointment and plans were made to replace with a Rotol model although this was never implemented. During a speed run with the engine limited to 3,000 rpm on 3 November, the Narval only reached {{cvt|560|km/h|0}} at {{cvt|5800|m}}. A week later the aircraft was flown to the Air Force's flight-test center at Brétigny for the service evaluation. The report was damning, judging its performance and stability inadequate, which meant that it would not be a good gun platform. The test pilots noted that the Narval tended to go into a dive when engine power was reduced, something that would make carrier landings very difficult, and that it demonstrated poor flying characteristics whenever the flap were retracted or extended.Buttler, pp. 85–86

The first prototype finally made its first flight on 9 December, the test pilot, Roger Carpentier, complaining that he had to struggle to keep the wings level in flight. During a flight on the second prototype on 16 December, Carpentier confirmed most of the official observations, commenting that he found it impossible to perform an aileron roll at a speed of {{cvt|460|km/h}}. Another pilot discovered that the first prototype behaved differently from the second one when the flaps were retracted, it banked to the right instead of diving. Flight testing ended on 7 January after the first prototype had only flown twice and the second one forty-four times for a total of 25 hours and 50 minutes of flight time. The aircraft were scrapped after the Narval program was cancelled in April. Contributing factors to the decision was the American delivery of Grumman F6F Hellcat and Vought F4U Corsair carrier fighters and that other French fighter projects used turbojets for power, which rendered the Narval fundamentally obsolete, despite a proposal by SNCASO in October 1948 to replace the Arsenal 12H with the British Rolls-Royce Nene turbojet as the SO.8010.Buttler, pp. 86–89

{{Aircraft specs

|ref=X-Planes of Europe II: Military Prototype Aircraft from the Golden Age 1946–1974Buttler, pp. 84, 87, 89

|prime units?=met

|genhide=

|crew=1

|capacity=

|length m=11.83

|length ft=

|length in=

|length note=

|span m=11.77

|span ft=

|span in=

|span note=

|height m=

|height ft=

|height in=

|height note=

|wing area sqm=26.3

|wing area sqft=

|wing area note=

|airfoil=

|empty weight kg=

|empty weight lb=

|empty weight note=

|gross weight kg=7261

|gross weight lb=

|gross weight note=

|max takeoff weight kg=

|max takeoff weight lb=

|max takeoff weight note=

|fuel capacity={{convert|1413|L|impgal USgal|adj=on}}

|lift note=

|more general=

|eng1 number=1

|eng1 name=Arsenal 12H-02

|eng1 type=water-cooled V-12 piston engine

|eng1 hp=2250

|eng1 note=

|power original=

|prop blade number=8

|prop name=contra-rotating Chauviére

|prop dia m=2.7

|prop dia note=

|perfhide=

|max speed kmh=730

|max speed mph=

|max speed kts=

|max speed note=(estimated) at {{cvt|8500|m}}

|cruise speed kmh=

|cruise speed mph=

|cruise speed kts=

|cruise speed note=

|stall speed kts=

|stall speed note=

|never exceed speed kmh=

|never exceed speed mph=

|never exceed speed kts=

|never exceed speed note=

|minimum control speed kmh=

|minimum control speed mph=

|minimum control speed kts=

|minimum control speed note=

|range km=

|range miles=

|range nmi=

|range note=

|combat range km=

|combat range miles=

|combat range nmi=

|combat range note=

|ferry range km=4500

|ferry range miles=

|ferry range nmi=

|ferry range note=

|endurance=

|ceiling m=10000

|ceiling ft=

|ceiling note=

|climb rate ms=

|climb rate ftmin=

|climb rate note=

|time to altitude=

|sink rate ms=

|sink rate ftmin=

|sink rate note=

|lift to drag=

|wing loading kg/m2=

|wing loading lb/sqft=

|wing loading note=

|power/mass=

|thrust/weight=

|more performance=

|guns= 6 × {{cvt|20|mm|1}} MG 151 autocannon

|bombs= {{cvt|1000|kg}}

|avionics=

}}

{{reflist}}

• Buttler, Tony. X-Planes of Europe II: Military Prototype Aircraft from the Golden Age 1945–1974. Manchester, UK: Hikoki Publications, 2015. {{ISBN|978-1-90210-948-0}}
• Carbonel, Jean-Christophe. French Secret Projects 1: Post War Fighters. Manchester, UK: Crecy Publishing, 2016 {{ISBN|978-1-91080-900-6}}
• {{cite web|last1=Pearce|first1=William|title=Sud-Ouest (SNCASO) SO.8000 Narval |url=https://oldmachinepress.com/2014/01/25/sud-ouest-sncaso-so-8000-narval/|website=oldmachinepress.com|access-date=2 February 2021}}

• {{cite journal |last1=Carbonel |first1=Jean-Christophe |title=Narval: The Dreaded SNCASO SO.8000|journal=The Aviation Historian |date=April 2018 |issue=23 |pages=76–87 |issn=2051-1930}}

• [http://www.flightglobal.com/pdfarchive/view/1949/1949%20-%200847.html Salon Studies ]Flight 12 May 1949

{{SNCASO aircraft}}

Category:Twin-boom aircraft

Category:Single-engined pusher aircraft

Category:1940s French fighter aircraft

Category:Aircraft with contra-rotating propellers

Narval

Category:Aircraft first flown in 1949

Category:Low-wing aircraft