IMAM Ro.30 - Development

Development

Following the success of earlier observation biplanes the Ro.30 was developed in 1932 for the Regia Aeronautica. It was an unequal-span biplane with a fixed tailwheel landing gear. It had an enclosed cockpit for the pilot located forward of the wing leading edge, an observer had a cabin between the wings, and the third crew member had an open cockpit behind the wings. It was powered either a 395kW (530hp) Alfa Romeo Mercury or a 373kW (530hp) Piaggio Jupiter radial engine.

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