Armstrong Siddeley Jaguar

Jaguar
Armstrong Siddeley Jaguar IV
Type Radial engine
National origin United Kingdom
Manufacturer Armstrong Siddeley
First run 21 June 1922

The Armstrong Siddeley Jaguar is an aircraft engine developed by Armstrong Siddeley. The Jaguar was a petrol-fuelled air-cooled 14-cylinder two-row radial engine design. The Jaguar III was first used in 1923, followed in 1925 by the Jaguar IV and in 1927 by the Jaguar VI. In 1925 the Jaguar became the first production aero engine incorporating a geared supercharger.[1]

  1. ^ "World Encyclopedia of Aero Engines – 5th edition" by Bill Gunston, Sutton Publishing, 2006. p.13