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- Rolls-Royce_RB401 abstract "The Rolls-Royce RB.401 was a two-spool business jet engine which Rolls-Royce started to develop in the mid-1970sas a replacement for the Viper.RB.401-06 prototype engines were already being manufactured when a decision to develop the higher thrust RB.401-07 was taken. Although ground testing of both the -06 and -07 continued into the early 1980s, a lack of funds caused the project to be cancelled.".
- Rolls-Royce_RB401 wikiPageID "3874102".
- Rolls-Royce_RB401 wikiPageRevisionID "591596808".
- Rolls-Royce_RB401 compression "~20:1".
- Rolls-Royce_RB401 diameter "32.4".
- Rolls-Royce_RB401 hasPhotoCollection Rolls-Royce_RB401.
- Rolls-Royce_RB401 lists "* List of aircraft engines".
- Rolls-Royce_RB401 manufacturer Rolls-Royce_Limited.
- Rolls-Royce_RB401 thrust "Take-off Thrust: 5,540 lbf, flat-rated to ISA+15C".
- Rolls-Royce_RB401 type Turbofan.
- Rolls-Royce_RB401 type "High bypass Turbofan".
- Rolls-Royce_RB401 subject Category:High-bypass_turbofan_engines.
- Rolls-Royce_RB401 subject Category:Rolls-Royce_aircraft_gas_turbine_engines.
- Rolls-Royce_RB401 subject Category:Turbofan_engines_1970–1979.
- Rolls-Royce_RB401 comment "The Rolls-Royce RB.401 was a two-spool business jet engine which Rolls-Royce started to develop in the mid-1970sas a replacement for the Viper.RB.401-06 prototype engines were already being manufactured when a decision to develop the higher thrust RB.401-07 was taken. Although ground testing of both the -06 and -07 continued into the early 1980s, a lack of funds caused the project to be cancelled.".
- Rolls-Royce_RB401 label "Rolls-Royce RB401".
- Rolls-Royce_RB401 sameAs m.0b4g1c.
- Rolls-Royce_RB401 sameAs Q17017089.
- Rolls-Royce_RB401 sameAs Q17017089.
- Rolls-Royce_RB401 wasDerivedFrom Rolls-Royce_RB401?oldid=591596808.
- Rolls-Royce_RB401 isPrimaryTopicOf Rolls-Royce_RB401.