French flying ace Georges Guynemer pushed the idea of a cannon-armed fighter plane after his experiences in aircraft such as the SPAD S.VII. This led the Societe Pour l'Aviation et ses Derives (SPAD) company to develop such a system. The follow-up design came to be known as the S.XII (or S.12) and featured a 37mm cannon along with its standard single machine gun armament.
Externally, the SPAD S.XII looked every bit as a further development of the SPAD S.VII model. Due to the extra weight imposed on the airframe by the new cannon armament, the fuselage was lengthened over that of the S.VII. A Hispano-Suiza engine was once again used by SPAD and consisted of the 8Bc or 8Bec types, each offering 220 horsepower. What made the 8Bec unique was that the 37mm cannon could be nestled between the cylinder banks. Subtle changes to the wings were also necessitated by the increase in weight.
First flight for the SPAD S.XII was achieved on July 5th, 1917 with limited production examples following. The system proved a handful for the inexperienced but lethal in the hands of a proven military aviator. As the cannon system extended into the cockpit, the aircraft was not controlled through a traditional flight stick. Additionally, reloading the cannon while flying the plane added another responsibility while in-flight. The standard single 7.7mm Vickers machine gun remained a part of the offensive toolbox for the S.XII, a carry-over from the S.VII design.
Though the cannon-mounted SPAD S.XII's initially proved successful, they really required an experienced pilot at the controls of both aircraft and armament. With more and more resources being dedicated to the already proven S.VII and S.XIII designs, the S.XII was limited to a mere 300 production examples and, as such, the system never equipped an entire unit. In any case, the idea of a cannon-armed aircraft was intriguing and perfected to the extreme in the Second World War and beyond.
Like the SPAD S.VII before it and the SPAD S.XIII after it, the SPAD S.XII was designed by Louis Bechereau.
Specifications
Year: 1917
Status Retired, Out-of-Service
Crew 1
[ 300 Units ] : Societe Pour l'Aviation et ses Derives (SPAD) - France
France; Imperial Russia; Serbia; United Kingdom; United States; Yugoslavia
- Fighter
Length:
21.00 ft (6.4 m)
Width:
26.25 ft (8 m)
Height:
8.37 ft (2.55 m)
(Showcased structural dimension values pertain to the SPAD S.XII production model)
Empty Weight:
1,294 lb (587 kg)
MTOW:
1,947 lb (883 kg)
(Diff: +653lb)
(Showcased weight values pertain to the SPAD S.XII production model)
1 x Hispano-Suiza HS 8Bc engine developing 220 horsepower OR 1 x Hispano-Suiza HS 8Bec engine developing 220 horsepower.
(Showcased powerplant information pertains to the SPAD S.XII production model)
Max Speed:
126 mph (203 kph; 110 kts)
Service Ceiling:
22,474 feet (6,850 m; 4.26 miles)
Max Range:
217 miles (350 km; 189 nm)
Rate-of-Climb:
1,090 ft/min (332 m/min)
(Showcased performance values pertain to the SPAD S.XII production model; Compare this aircraft entry against any other in our database)
STANDARD:
1 x 7.7mm Vickers machine gun
Some with HS 8Bec engines featured a 1 x 37mm Puteaux cannon mounted between the cylinder banks.
(Showcased armament details pertain to the SPAD S.XII production model)
S.XII - Base Series Designation
* Ribbons not necessarily indicative of actual historical campaign ribbons. Ribbons are clickable to their respective campaigns/operations.
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France; Imperial Russia; Serbia; United Kingdom; United States; Yugoslavia
