The SNCASO SO.4000 was an
experimental French twin-engine
bomber
A bomber is a military combat aircraft designed to attack ground and naval targets by dropping air-to-ground weaponry (such as bombs), launching aerial torpedo, torpedoes, or deploying air-launched cruise missiles. The first use of bombs dropped ...
of the 1950s. It was the first French jet bomber developed, but it never entered operational service.
The SO.4000 was developed because the
French Air Force
The French Air and Space Force (AAE) (french: Armée de l'air et de l'espace, ) is the air and space force of the French Armed Forces. It was the first military aviation force in history, formed in 1909 as the , a service arm of the French Army; ...
needed a jet bomber, which produced a specification calling for one after the end of
Second World War
World War II or the Second World War, often abbreviated as WWII or WW2, was a world war that lasted from 1939 to 1945. It involved the vast majority of the world's countries—including all of the great powers—forming two opposin ...
. The SNCASO's SO.4000 received a development contract to produce a pair of mockups and a full-scale
prototype
A prototype is an early sample, model, or release of a product built to test a concept or process. It is a term used in a variety of contexts, including semantics, design, electronics, and Software prototyping, software programming. A prototyp ...
. The single full-scale aircraft, which performed its first and only test flight on 15 March 1951, would never enter mass production. Even prior to this flight, the design had been made obsolete by rapid advances in the field of aviation and was overweight and underpowered. Shortly after its only flight, during which it had been damaged during the landing, it was decided to abandon development. However, the SO.4000 would form the basis of the far more successful
SO.4050 Vautour.
["IAF Aircraft Inventory: Sud-Ouest S.O. 4050 Vautour."](_blank)
Jewish Virtual Library, Retrieved: 16 September 2017.
Development
France's aviation industry was in dire straits, having been damaged more heavily than any other Allied nation as a consequence of the
Second World War
World War II or the Second World War, often abbreviated as WWII or WW2, was a world war that lasted from 1939 to 1945. It involved the vast majority of the world's countries—including all of the great powers—forming two opposin ...
.
[Caygill 2006, .] Regardless, the French needed to revive the nation's aviation industry, and to use the latest advances for a new generation of competitive locally-built aircraft. France, like other
Allied nations
The Allies, formally referred to as the United Nations from 1942, were an international military coalition formed during the Second World War (1939–1945) to oppose the Axis powers, led by Nazi Germany, Imperial Japan, and Fascist Italy. ...
in the war, benefitted from captured German research into high speed aircraft.
These efforts were also aimed at reducing France's reliance on imported technology, and looked at
jet propulsion and
transonic
Transonic (or transsonic) flow is air flowing around an object at a speed that generates regions of both subsonic and supersonic airflow around that object. The exact range of speeds depends on the object's critical Mach number, but transonic ...
aerodynamics
Aerodynamics, from grc, ἀήρ ''aero'' (air) + grc, δυναμική (dynamics), is the study of the motion of air, particularly when affected by a solid object, such as an airplane wing. It involves topics covered in the field of fluid dyn ...
.
Following the end of the war, the
French Air Force
The French Air and Space Force (AAE) (french: Armée de l'air et de l'espace, ) is the air and space force of the French Armed Forces. It was the first military aviation force in history, formed in 1909 as the , a service arm of the French Army; ...
produced a requirement for a jet bomber which was expected to have a takeoff weight of roughly and be capable of
transonic
Transonic (or transsonic) flow is air flowing around an object at a speed that generates regions of both subsonic and supersonic airflow around that object. The exact range of speeds depends on the object's critical Mach number, but transonic ...
speeds. The development of a jet-powered bomber aircraft was viewed as being a major technological challenge and this initiative would produce the first French jet bomber in the form of the SO.4000.
[Gunston and Gilchrist 1993, p. 68.]
Submissions were tendered by several French aircraft manufacturers, including
SNCASO with the SO 4000 and
SNCAC's rival bid in the form of the
SNCAC NC 270. Following a competitive review, SNCASO would receive a development order calling for a pair of manned scale models and a full-sized
prototype
A prototype is an early sample, model, or release of a product built to test a concept or process. It is a term used in a variety of contexts, including semantics, design, electronics, and Software prototyping, software programming. A prototyp ...
. The first scale model, known as the ''SNCASO M.1'', was an unpowered
glider
Glider may refer to:
Aircraft and transport Aircraft
* Glider (aircraft), heavier-than-air aircraft primarily intended for unpowered flight
** Glider (sailplane), a rigid-winged glider aircraft with an undercarriage, used in the sport of glidin ...
which would be tested from atop the
Heinkel He 274 V1, (as the French AAS 01A), the first prototype of a late-war high-altitude
strategic bomber
A strategic bomber is a medium- to long-range penetration bomber aircraft designed to drop large amounts of air-to-ground weaponry onto a distant target for the purposes of debilitating the enemy's capacity to wage war. Unlike tactical bombers, ...
, which had remained in France after the war. The He 274, having drawn the attention of French authorities, had been restored to flightworthy condition to allow such use. The second aircraft, the
SNCASO M.2, was powered by a single
British Rolls-Royce Derwent turbojet
The turbojet is an airbreathing jet engine which is typically used in aircraft. It consists of a gas turbine with a propelling nozzle. The gas turbine has an air inlet which includes inlet guide vanes, a compressor, a combustion chamber, and ...
engine. SNCAC also received a contract to produce a prototype for their submission.
["Le Sud-Ouest SO-4000: I. Origine"](_blank)
''Le Sit des Projets et Prototypes d'Avions'', 14 May 2003. Retrieved 15 May 2011.
During 1947, as a result of the rapid advances made in aviation technologies made around this time, plans for a subsequent production run were abandoned. Nevertheless, it was decided to complete the two scale models and the full size prototype for experimental purposes.
''Le Sit des Projets et Prototypes d'Avions'', 14 May 2003. Retrieved 15 May 2011. On 13 April 1949, the sole M.2 conducted its maiden flight
The maiden flight, also known as first flight, of an aircraft is the first occasion on which it leaves the ground under its own power. The same term is also used for the first launch of rockets.
The maiden flight of a new aircraft type is alwa ...
, while the M.1 glider performed its first free-flight, launched from a SNCASE Languedoc
The SNCASE SE.161 Languedoc was a French four-engined airliner produced by SNCASE (Sud-Est). Developed from the Bloch MB.160 and known in the late 1930s as the (SNCSO) Bloch MB.161, the SE.161 was in service with Air France and the French milita ...
, on 26 September 1949. Testing of the M.2 was considered to be successful, on one occasion having exceeded 1,000 km/h (621 mph) while flown in a dive, becoming the first French aircraft to achieve this feat. Both the M.1 and M.2 provided valuable data on features such as swept wing
A swept wing is a wing that angles either backward or occasionally forward from its root rather than in a straight sideways direction.
Swept wings have been flown since the pioneer days of aviation. Wing sweep at high speeds was first investigate ...
s, pilot escape systems, spoiler
Spoiler is a security vulnerability on modern computer central processing units that use speculative execution. It exploits side-effects of speculative execution to improve the efficiency of Rowhammer and other related memory and cache attacks. Ac ...
control, and leading edge
The leading edge of an airfoil surface such as a wing is its foremost edge and is therefore the part which first meets the oncoming air.Crane, Dale: ''Dictionary of Aeronautical Terms, third edition'', page 305. Aviation Supplies & Academics, ...
slat
Slat, slats, or SLAT may refer to:
* Slat (aircraft), aerodynamic surfaces on the leading edge of the wings of fixed-wing aircraft
* a Lath, a narrow strip of straight-grained wood used under roof shingles or tiles
* Vertical or horizontal pieces ...
s.
On 5 March 1950, the SO.4000 was rolled out; by this point, it was already obsolete and lacking in capabilities compared to its contemporaries. During the following month, the aircraft sustained damage when its undercarriage
Undercarriage is the part of a moving vehicle that is underneath the main body of the vehicle. The term originally applied to this part of a horse-drawn carriage, and usage has since broadened to include:
*The landing gear of an aircraft.
*The ch ...
collapsed during taxiing tests. After completing repairs, the SO.4000 performed its maiden flight on 15 March 1951, piloted by chief test pilot Jaques Guignard. During landing, its undercarriage failed again, resulting in damage. The aircraft would never fly again and work on the project was abandoned without any further testing being carried out. According to Gunston and Gilchrist, the SO.4000 was a very heavy aircraft, which only compounded the weakness of possessing relatively little engine power, giving it an extremely poor thrust-to-weight ratio even when empty; they also criticised it as possessing "useless capabilities".[Gunston and Gilchrist 1993, p. 69.]
Design
The SO.4000 was an unconventional experimental jet bomber. It featured a mid-mounted wing, which was swept at an angle of 35 degrees and mated with a carefully streamlined oval-section fuselage
The fuselage (; from the French ''fuselé'' "spindle-shaped") is an aircraft's main body section. It holds crew, passengers, or cargo. In single-engine aircraft, it will usually contain an engine as well, although in some amphibious aircraft t ...
, which was furnished with a relatively tall tricycle undercarriage
Tricycle gear is a type of aircraft undercarriage, or ''landing gear'', arranged in a tricycle fashion. The tricycle arrangement has a single nose wheel in the front, and two or more main wheels slightly aft of the center of gravity. Tricycle ge ...
. This undercarriage, which was provisioned with tandem mainwheels, was somewhat unorthodox, as they retracted outwards into alcoves cut into perhaps the most stressed area of the airframe. The aircraft was powered by a pair of Rolls-Royce Nene
The Rolls-Royce RB.41 Nene is a 1940s British centrifugal compressor turbojet engine. The Nene was a complete redesign, rather than a scaled-up Rolls-Royce Derwent"Rolls-Royce Aero Engines" Bill Gunston, Patrick Stephens Limited 1989, , p.111 w ...
turbojet engines, each capable of generating a maximum of 22.2 kN (4,980 lbf); Gunston and Gilchrist note the use of the Nene to be one of the few conventional choices adopted for the design. These engines were mounted in a side-by-side arrangement housed within the rear fuselage. Inlets for the engine were located on either side of the forward fuselage, while boundary layer air was directed via a splitter to slits above and below the lengthy inlet duct. The tailpipes were somewhat unusual, the nozzles being separated by the aircraft's fin
A fin is a thin component or appendage attached to a larger body or structure. Fins typically function as foils that produce lift or thrust, or provide the ability to steer or stabilize motion while traveling in water, air, or other fluids. Fin ...
.
The SO.4000 was operated by a crew of two, consisting of a pilot and test engineer/observer, both of which were seated in a pressurised
{{Wiktionary
Pressurization or pressurisation is the application of pressure in a given situation or environment.
Industrial
Industrial equipment is often maintained at pressures above or below atmospheric.
Atmospheric
This is the process by ...
cockpit located within the extreme nose of the aircraft and covered by a conventional canopy.[Gunston and Gilchrist 1993, pp. 68-69.][''Flight'' 12 May 1949, p. 552.] All of the flight surfaces were manually-actuated, although powered counterparts were envisioned for subsequent aircraft. A hydraulic system was used for some moving elements, such as the undercarriage and the flaps. Being intended for use as a bomber, the (unbuilt) production aircraft were envisioned to be capable of carrying a bombload of up to 5,000 kg (11,000 lb); furthermore, it was planned to install remotely-controlled barbette
Barbettes are several types of gun emplacement in terrestrial fortifications or on naval ships.
In recent naval usage, a barbette is a protective circular armour support for a heavy gun turret. This evolved from earlier forms of gun protection ...
s that would have been armed with a pair of 20 mm cannon
A cannon is a large- caliber gun classified as a type of artillery, which usually launches a projectile using explosive chemical propellant. Gunpowder ("black powder") was the primary propellant before the invention of smokeless powder ...
on the wingtips.["Le Sud-Ouest SO-4000: II. Le NC-270 & le SO-4000"](_blank)
''Le Sit des Projets et Prototypes d'Avions''. 14 May 2003. Retrieved 15 May 2011. The bomb bay would have been installed within the centre fuselage underneath the wing's central section. Despite its large size, the SO.4000's total fuel capacity was 1,430 gallons, which would have severely restricted its operational range if the type had ever entered service.
Variants
;SNCASO M1:A scale unpowered glider for research into the flying characteristics of the full size S.O.4000. Launched from a support frame above the fuselage of the sole Heinkel He 274, which had been abandoned in France and restored to airworthiness to support research programmmes, and/or a similarly equipped SE-161 Languedoc.
;SNCASO M2:Essentially similar to the M1 but powered by a single Rolls-Royce Derwent V
The Rolls-Royce RB.37 Derwent is a 1940s British centrifugal compressor turbojet engine, the second Rolls-Royce jet engine to enter production. It was an improved version of the Rolls-Royce Welland, which itself was a renamed version of Frank ...
centrifugal flow turbojet engine. First flown on 13 April 1949.
;SNCASO S.O.4000:A single prototype of this jet powered bomber first flown on 15 March 1951. Powered by 2 × Rolls-Royce Nene 102
The Rolls-Royce RB.41 Nene is a 1940s British centrifugal compressor turbojet engine. The Nene was a complete redesign, rather than a scaled-up Rolls-Royce Derwent"Rolls-Royce Aero Engines" Bill Gunston, Patrick Stephens Limited 1989, , p.111 w ...
centrifugal flow turbojet engines.
Specifications (Performance estimated)
References
Citations
Bibliography
* "An Abortive Bomber". ''Air International
''AIR International'' is a British aviation magazine covering current defence aerospace and civil aviation topics. It has been in publication since 1971 and is currently published by Key Publishing Ltd.
History and profile
The magazine was fir ...
'', January 1986, Vol 30 No 1. Bromley, UK: Fine Scroll. p. 46. ISSN 0306-5634.
* Buttler, Tony. ''X-Planes of Europe II: Military Prototype Aircraft from the Golden Age 1946–1974''. Manchester, UK: Hikoki Publications, 2015.
* Caygill, Peter. ''Sound Barrier: The Rocky Road to MACH 1.0+''. Pen and Sword, 2006.
*
* Gunston, Bill and Peter Gilchrist. ''Jet Bombers: From the Messerschmitt Me 262 to the Stealth B-2''. Osprey, 1993.
External links
Aviafrance
{{SNCASO aircraft
1950s French bomber aircraft
SO.4000