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- Rolls-Royce_RB162 abstract "The Rolls-Royce RB.162 was a simply constructed and lightweight British turbojet engine produced by Rolls-Royce Limited. Developed in the early 1960s, it was specially designed for use as a lift engine for VTOL aircraft but was also used in a later variant of the Hawker Siddeley Trident airliner as an auxiliary boost engine. A smaller related variant, the RB.181 remained a design project only, as did a turbofan version designated RB.175.".
- Rolls-Royce_RB162 wikiPageExternalLink rb162.php.
- Rolls-Royce_RB162 wikiPageExternalLink 106%20Rolls%20Royce%20RB162%20engine.htm.
- Rolls-Royce_RB162 wikiPageExternalLink 1963%20-%200951.html.
- Rolls-Royce_RB162 wikiPageExternalLink rb162-86.jpg.
- Rolls-Royce_RB162 wikiPageExternalLink www.zulukilo.org.uk.
- Rolls-Royce_RB162 wikiPageID "20417761".
- Rolls-Royce_RB162 wikiPageRevisionID "575487039".
- Rolls-Royce_RB162 aircon "86".
- Rolls-Royce_RB162 combustion "Annular".
- Rolls-Royce_RB162 compressor "6".
- Rolls-Royce_RB162 diameter "25.0".
- Rolls-Royce_RB162 firstRun "January".
- Rolls-Royce_RB162 hasPhotoCollection Rolls-Royce_RB162.
- Rolls-Royce_RB162 length "51.6".
- Rolls-Royce_RB162 lists "*List of aircraft engines".
- Rolls-Royce_RB162 majorApplications Dornier_Do_31.
- Rolls-Royce_RB162 majorApplications Hawker_Siddeley_Trident.
- Rolls-Royce_RB162 manufacturer Rolls-Royce_Limited.
- Rolls-Royce_RB162 numberBuilt "86".
- Rolls-Royce_RB162 seeAlso "*Rolls-Royce Thrust Measuring Rig".
- Rolls-Royce_RB162 similarEngines "*Armstrong Siddeley Viper *Bristol Siddeley Orpheus *Rolls-Royce RB108".
- Rolls-Royce_RB162 thrust "5250.0".
- Rolls-Royce_RB162 weight "18.75".
- Rolls-Royce_RB162 turbine "Single-stage axial flow".
- Rolls-Royce_RB162 type Turbojet.
- Rolls-Royce_RB162 type "Single spool turbojet".
- Rolls-Royce_RB162 weight "280.0".
- Rolls-Royce_RB162 subject Category:Rolls-Royce_aircraft_gas_turbine_engines.
- Rolls-Royce_RB162 subject Category:Turbojet_engines_1960–1969.
- Rolls-Royce_RB162 comment "The Rolls-Royce RB.162 was a simply constructed and lightweight British turbojet engine produced by Rolls-Royce Limited. Developed in the early 1960s, it was specially designed for use as a lift engine for VTOL aircraft but was also used in a later variant of the Hawker Siddeley Trident airliner as an auxiliary boost engine. A smaller related variant, the RB.181 remained a design project only, as did a turbofan version designated RB.175.".
- Rolls-Royce_RB162 label "Rolls-Royce RB.162".
- Rolls-Royce_RB162 label "Rolls-Royce RB162".
- Rolls-Royce_RB162 label "Rolls-Royce RB162".
- Rolls-Royce_RB162 label "ロールス・ロイス RB162".
- Rolls-Royce_RB162 sameAs Rolls-Royce_RB.162.
- Rolls-Royce_RB162 sameAs Rolls-Royce_RB162.
- Rolls-Royce_RB162 sameAs ロールス・ロイス_RB162.
- Rolls-Royce_RB162 sameAs m.04zwzmm.
- Rolls-Royce_RB162 sameAs Q1162032.
- Rolls-Royce_RB162 sameAs Q1162032.
- Rolls-Royce_RB162 wasDerivedFrom Rolls-Royce_RB162?oldid=575487039.
- Rolls-Royce_RB162 isPrimaryTopicOf Rolls-Royce_RB162.