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- Turbomeca_Bastan abstract "The Turbomeca Bastan was a turboprop engine developed in France in 1957. Early models developed 650 shp (485 kW), but by 1965 this had been increased to 1,048 shp (780 kW) with the Bastan VII. Flight tests of some Bastan models were carried out using a Lockheed Constellation flying test bed. The engine's principal applications were the Aérospatiale N 262 (Nord 262) and Nord 260 airliners.The Bastan was also developed into the Turbomeca Aubisque turbofan.".
- Turbomeca_Bastan wikiPageID "10195198".
- Turbomeca_Bastan wikiPageRevisionID "590236560".
- Turbomeca_Bastan combustion "Direct flow annular type".
- Turbomeca_Bastan compression "5.83".
- Turbomeca_Bastan compressor "Single-stage axial compressor followed by single-stage centrifugal compressor".
- Turbomeca_Bastan developedInto Turbomeca_Aubisque.
- Turbomeca_Bastan diameter "685".
- Turbomeca_Bastan hasPhotoCollection Turbomeca_Bastan.
- Turbomeca_Bastan length "2034.0".
- Turbomeca_Bastan lists "*List of aircraft engines".
- Turbomeca_Bastan majorApplications Aérospatiale_N_262.
- Turbomeca_Bastan majorApplications "Nord 260".
- Turbomeca_Bastan manufacturer Turbomeca.
- Turbomeca_Bastan nationalOrigin "France".
- Turbomeca_Bastan power "794.0".
- Turbomeca_Bastan weight "3.7".
- Turbomeca_Bastan ref "Janes's All The World's Aircraft 1965-66.".
- Turbomeca_Bastan related "* Turbomeca Aubisque".
- Turbomeca_Bastan specfuelcon "352".
- Turbomeca_Bastan turbine "Three-stage axial flow".
- Turbomeca_Bastan type Turboprop.
- Turbomeca_Bastan weight "212.0".
- Turbomeca_Bastan subject Category:Turbomeca_aircraft_engines.
- Turbomeca_Bastan subject Category:Turboprop_engines_1950–1959.
- Turbomeca_Bastan type AircraftEngine102687423.
- Turbomeca_Bastan type Artifact100021939.
- Turbomeca_Bastan type Device103183080.
- Turbomeca_Bastan type Engine103287733.
- Turbomeca_Bastan type Instrumentality103575240.
- Turbomeca_Bastan type Machine103699975.
- Turbomeca_Bastan type Motor103789946.
- Turbomeca_Bastan type Object100002684.
- Turbomeca_Bastan type PhysicalEntity100001930.
- Turbomeca_Bastan type TurbomecaAircraftEngines.
- Turbomeca_Bastan type Whole100003553.
- Turbomeca_Bastan comment "The Turbomeca Bastan was a turboprop engine developed in France in 1957. Early models developed 650 shp (485 kW), but by 1965 this had been increased to 1,048 shp (780 kW) with the Bastan VII. Flight tests of some Bastan models were carried out using a Lockheed Constellation flying test bed. The engine's principal applications were the Aérospatiale N 262 (Nord 262) and Nord 260 airliners.The Bastan was also developed into the Turbomeca Aubisque turbofan.".
- Turbomeca_Bastan label "Turbomeca Bastan".
- Turbomeca_Bastan label "Turbomeca Bastan".
- Turbomeca_Bastan sameAs Turbomeca_Bastan.
- Turbomeca_Bastan sameAs m.02q4trv.
- Turbomeca_Bastan sameAs Q4000566.
- Turbomeca_Bastan sameAs Q4000566.
- Turbomeca_Bastan sameAs Turbomeca_Bastan.
- Turbomeca_Bastan wasDerivedFrom Turbomeca_Bastan?oldid=590236560.
- Turbomeca_Bastan isPrimaryTopicOf Turbomeca_Bastan.