The RB.106 was a two-shaft design with two axial flow compressors each driven by its own single stage turbine and
reheat. It was of similar size to the
Rolls-Royce Avon, allowing it to be used as a drop-in replacement, but it would have produced about twice the thrust (with reheat) at 21,750 lbf (96.7 kN). The two-shaft layout was relatively advanced for the era; the single-shaft
de Havilland Gyron matched it in power terms, while the two-spool
Bristol Olympus was much less powerful at its then-current state of development. Apart from being expected to power British aircraft such as those competing for
Operational Requirement F.155, it was selected to be the powerplant for the
Avro Canada CF-105 Arrow. The American company
Westinghouse was reported in 1956 to be serious about acquiring a licence to build the RB.106. A scaled-up version of the RB.106 intended for F.155 was the
Rolls-Royce RB.122. The competing
Bristol two-spool engine to the same specification was to have been the
Bristol Zeus. However funding was cut with the
1957 Defence White Paper which terminated most aircraft development then under way. The Arrow moved to an indigenous two-spool design similar to the RB.106, the
Orenda Iroquois. ==Applications (proposed)==