Sopwith Salamander

It was a single-engined, single-seat biplane, based on the Sopwith Snipe fighter, with an armoured forward fuselage to protect the pilot and fuel system from ground fire during low level operations.

It was ordered in large numbers for the Royal Air Force but the war ended before the type could enter squadron service, although two were in France in October 1918.

In August 1917, the British Royal Flying Corps (RFC) introduced the coordinated mass use of single-seat fighter aircraft for low-level ground-attack operations in support of the Third Battle of Ypres, with Airco DH.5s, which were unsuitable for high-altitude combat, specialising in this role.

The tactic proved effective and was repeated at the Battle of Cambrai in November 1917 by DH.5s and Sopwith Camels being used in strafing attacks.

[1][4] As a result of the high losses sustained during strafing and after seeing the success of the new German types, the RFC instructed the Sopwith Aviation Company to modify a Camel for close air support, by fitting downward-firing guns and armour.

[7] The rear (unarmoured) section of the fuselage was a generally similar structure to the Snipe but flat sided, to match the forepart.

The new aircraft used the same Bentley BR2 rotary engine as the Snipe, covered by an unarmoured cowling – the foremost armour plate forming the firewall.

[14] Production was slowed, however, by problems producing the armour plate, this being prone to distortion during the hardening process,[12] and shortages of the BR.2 engine.

Side view of third prototype Salamander