Salmson 2

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Military reconnaissance aircraft

title: "Salmson 2" type: doc version: 1 created: 2026-02-28 author: "Wikipedia contributors" status: active scope: public tags: ["1910s-french-military-reconnaissance-aircraft", "biplanes", "salmson-aircraft", "single-engined-tractor-aircraft", "aircraft-first-flown-in-1917", "aircraft-with-fixed-conventional-landing-gear"] description: "Military reconnaissance aircraft" topic_path: "geography/france" source: "https://en.wikipedia.org/wiki/Salmson_2" license: "CC BY-SA 4.0" wikipedia_page_id: 0 wikipedia_revision_id: 0

::summary Military reconnaissance aircraft ::

::data[format=table title="Infobox aircraft"]

FieldValue
nameSalmson 2 A.2
imageFile:Salmson 2 WW1 recon aircraft.jpg
typeReconnaissance biplane
manufacturerSalmson
first_flight1917
number_built3,800+
::

|name= Salmson 2 A.2 |image= File:Salmson 2 WW1 recon aircraft.jpg |caption= |type= Reconnaissance biplane |manufacturer= Salmson |designer= |first_flight= 1917 |introduction= |retired= |number_built=3,800+ |status= |primary_user= |more_users= |unit cost= |variants=

The Salmson 2 A.2, (often shortened to Salmson 2) was a French biplane reconnaissance aircraft developed and produced by Salmson to a 1916 requirement. Along with the Breguet 14, it was the main reconnaissance aircraft of the French army in 1918 and was also used by American Expeditionary Force aviation units. At the end of the First World War, one-third of French reconnaissance aircraft were Salmson 2s.

Design and development

During the First World War, the Salmson factory built aircraft engines, generally 9- and later 18-cylinder water-cooled radial engines developed from the Swiss Canton-Unné design, an early stationary radial engine design used for military aircraft. The company's first aircraft was the Salmson-Moineau S.M.1, an unusual three-seat reconnaissance biplane with twin propellers gear-driven from a single Salmson engine mounted sideways in the fuselage but it was not successful although it saw limited production.

The Salmson 2 came from a requirement to replace the Sopwith 1½ Strutter and Dorand A.R. reconnaissance aircraft in the A.2 (tactical reconnaissance) role. Salmson had built the 1½ Strutter under license, and the Salmson 2, while an original design, had more in common with the Sopwith than to the Salmson-Moineau. The aircraft was of conventional construction with a two-bay biplane configuration, powered by the company's own 230 hp Salmson 9Z water-cooled radial engine. Some minor control problems were quickly resolved in early testing, but the main defect of the Salmson 2, shared with the contemporary Airco DH.4, was that the pilot and gunner were widely separated, making communication difficult. Production was ordered after trials on 29 April 1917, and deliveries were underway by October of that year. Around 3,200 Salmson 2s were built in France, 2,200 by Salmson and the remainder by the Latécoère, Hanriot, and Desfontaines, companies. Some of these were Salmson 2 E.2 dual control advanced training (Ecole) aircraft.

::figure[src="https://upload.wikimedia.org/wikipedia/commons/e/e8/Salmson_2_Limousine_L'Aéronautique_October_1921.jpg" caption="Salmson 2 Limousine photo from L'Aéronautique October 1921"] ::

::figure[src="https://upload.wikimedia.org/wikipedia/commons/6/63/Lignes_Aeriennes_Latécoére_(Latécoére-Toulouse).jpg" caption="Salmson 2 Berline of Lignes Aeriennes Latécoére, ''circa ''1918"] ::

Variants

Developments of the Salmson 2 included:

  • Salmson 2 A.2 standard model.
  • Salmson 2 E.2 dual control advanced training aircraft.
  • Salmson 4 Ab.2 was an enlarged version fitted with armour to meet the ground attack role. Production in 1918 was limited, and was cancelled at the end of the war.
  • Salmson 5 A.2 was a modified Salmson 2, with no production.
  • Salmson 7 A.2 was a modified Salmson 2. The primary change was that the pilot and gunner were seated back-to-back in a single cockpit. Large scale production was planned, but was cancelled with the end of the war.
  • Salmson Limousine ex-military Salmson 2s converted into enclosed civilian passenger aircraft after the First World War.
  • Salmson 2 Berline ex-military Salmson 2s converted into open cockpit civilian passenger aircraft after the First World War.
  • Kawasaki Army Otsu-1 (乙-1) Reconnaissance Aircraft was a Japanese licence-built Salmson 2 A.2.

Operational history

In addition to its service with the French army, the Salmson 2 served during the First World War with United States air units. Some 700 were purchased, and were generally successful.

Postwar Salmson 2s were purchased by Czechoslovakia, and remained in service until 1924. Others were transferred to Poland, but were withdrawn by 1920, and replaced by Bristol F.2Bs. Japan undertook licensed production as the '*Army Type *Otsu 1''''', also known as the Kawasaki-Salmson. The number of aircraft built in Japan is unclear; 300 were built by Kawasaki, and the same quantity by the Imperial Japanese Army's Tokorozawa supply depot, although the total number of aircraft produced may have been as high as 1,000.

After First World War, the Salmson 2 A.2 produced by Latécoère were the first aircraft used by French pioneering airmail company Aéropostale.

Military operators

Wartime

;

Post-war

::figure[src="https://upload.wikimedia.org/wikipedia/commons/2/21/Otusiki_1gata_teisatuki.jpg" caption="Japanese ''Otsu-1''"] ::

;

Aircraft on display

File:かかみがはら航空宇宙科学博物館 (21174615321).jpg|Replica Salmson 2 A.2/Otsu 1 in Japan. File:Replica Salmson 2 A.2 at Envol des pionniers.jpg|Replica Salmson 2 A.2 in Toulouse, France.

Specifications

::figure[src="https://upload.wikimedia.org/wikipedia/commons/3/39/Salmson_2_A.2_dwg.jpg" caption="Salmson 2 A.2 drawing"] ::

|ref=French Aircraft of the First World War |prime units?=met General characteristics

|crew=2 |length m=8.5 |length note= |span m=11.75 |span note= |height m=2.9 |height note= |wing area sqm=37.27 |wing area note= |aspect ratio= |airfoil= |empty weight kg=780 |empty weight note= |gross weight kg=1290 |gross weight note= |max takeoff weight kg= |max takeoff weight note= |fuel capacity= |more general= Powerplant

|eng1 number=1 |eng1 name=Salmson 9Za |eng1 type=9-cylinder water-cooled radial piston engine |eng1 kw=172 |eng1 note=

|prop blade number=2 |prop name=fixed-pitch propeller |prop dia m= |prop dia note= Performance

|max speed kmh=188 |max speed note=at sea level |cruise speed kmh= |cruise speed note= |stall speed kmh= |stall speed note= |never exceed speed kmh= |never exceed speed note= |range km=500 |range note= |combat range km= |combat range note= |ferry range km= |ferry range note= |endurance= |ceiling m=6250 |ceiling note= |climb rate ms= |climb rate note= |time to altitude=2,000 m in 7 minutes 13 seconds |wing loading kg/m2= |wing loading note= |fuel consumption kg/km= |power/mass= |thrust/weight= |more performance=

  • Take-off run: m
  • Take-off distance to 15 m: m
  • Landing run: m
  • Landing distance from 15 m: m-- Armament -- |guns=*

|avionics=

References

Bibliography

References

  1. (1997). "French Aircraft of the First World War". Flying Machines Press.
  2. Owers, Colin A.. (2001). "Salmson aircraft of World War I". Paladin Press.

::callout[type=info title="Wikipedia Source"] This article was imported from Wikipedia and is available under the Creative Commons Attribution-ShareAlike 4.0 License. Content has been adapted to SurfDoc format. Original contributors can be found on the article history page. ::

1910s-french-military-reconnaissance-aircraftbiplanessalmson-aircraftsingle-engined-tractor-aircraftaircraft-first-flown-in-1917aircraft-with-fixed-conventional-landing-gear