The SAAB J 21 needed a top speed of at least , which required a powerful engine. It was decided to substitute the Taurus engine for the American
Pratt & Whitney R-1830 Twin Wasp radial engine. The SAAB 21 was an unorthodox
twin-boom low wing
pusher configuration fighter aircraft with a
tricycle landing gear, and a heavy forward-firing armament. Several recent innovations were incorporated into its design, including an
ejection seat for the pilot while the pusher layout later allowed the type to be readily re-engined with a
turbojet. The advantages of a pusher design include an unobstructed forward view for the pilot, and the armament can be concentrated in the nose, however, a major drawback is difficulty in making an emergency exit as the pilot could get drawn into the propeller blades. Many solutions were examined, such as jettisoning either the propeller or the engine via explosive charges prior to bailing out, before it was decided to adopt an
ejection seat developed by Swedish defense firm
Bofors, in parallel with the fighter. The J 21 was one of the first operational aircraft in the world with an ejection seat. Swedish Air Force enthusiasm for a jet fighter in late 1945 pushed SAAB to produce a version of the J 21 using
jet propulsion. At Swedish Air Force request, existing J 21 aircraft were converted to jet propulsion in 1947 and redesignated
J 21R. This required modifications to over 50 per cent of the airframe, including the tailplane and wing. The aircraft was to be powered by a single British-sourced
de Havilland Goblin turbojet engine, to replace the DB 605B. It entered Swedish Air Force service as their first jet aircraft. ==Operational history==