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Rolls-Royce RB401

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The RB401 was business jet engine which Rolls-Royce started to develop in the mid-1970's.

RB401-06 prototype engines were already being manufactured when a decision to develop the higher thrust RB401-07 was taken.

Although the basic configurations of both engines were almost identical, the -07 variant had a larger fan diameter. A single stage fan, driven by 2 stage LP turbine, supercharged an 8 stage HP compressor, driven by a single stage transonic HP turbine. The combustor was annular and the co-annular exhaust featured a lightweight target type thrust reverser.

Leading particulars for -07 variant were as follows:

Fan Diameter: 32.4in

Take-off Thrust: 5540lbf, flat-rated to ISA+15C

Cruise Thrust: 1128lbf (Mach 0.7, 40000ft, ISA+10C)

Although ground testing of both the -06 and -07 continued into the early 80's, a lack of funds caused the project to be cancelled.

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