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- Reaction_Engines_A2 abstract "The Reaction Engines Limited A2 (called the A2) is a design study for a hypersonic airliner intended to provide environmentally friendly, long range, high capacity commercial transportation. The aircraft is being examined as part of the LAPCAT programme of the European Union, but has not yet been commercially launched, though the British design firm Reaction Engines Limited says it could be developed into a working aircraft within 25 years once there is market demand for it.".
- Reaction_Engines_A2 designer Reaction_Engines_Limited.
- Reaction_Engines_A2 type Hypersonic_speed.
- Reaction_Engines_A2 wikiPageExternalLink www.reactionengines.co.uk.
- Reaction_Engines_A2 wikiPageExternalLink vid_lapcat.html.
- Reaction_Engines_A2 wikiPageID "15607775".
- Reaction_Engines_A2 wikiPageRevisionID "602014516".
- Reaction_Engines_A2 areaMain "900".
- Reaction_Engines_A2 capacity "300".
- Reaction_Engines_A2 cruiseSpeedAlt "6400.0".
- Reaction_Engines_A2 cruiseSpeedMain "Mach 5.2".
- Reaction_Engines_A2 designer Reaction_Engines_Limited.
- Reaction_Engines_A2 engine(jet)_ Reaction_Engines_Scimitar.
- Reaction_Engines_A2 hasPhotoCollection Reaction_Engines_A2.
- Reaction_Engines_A2 jetOrProp%3F_ "jet".
- Reaction_Engines_A2 manufacturer "Undetermined".
- Reaction_Engines_A2 maxTakeoffWeightMain "400000.0".
- Reaction_Engines_A2 moreGeneral "Fuel capacity: 198 tonnes liquid hydrogen".
- Reaction_Engines_A2 morePerformance "*Specific fuel consumption: 0.86 lb/lbf·h at Mach 5 , 0.38 lb/lbf·h at Mach 0.9 *Lift to drag ratio: 11.0 at 5.9 km, Mach 0.9; 5.9 at 25 km, Mach 5 *Noise: 101 dBa at 450 m lateral".
- Reaction_Engines_A2 numberOfJets "4".
- Reaction_Engines_A2 planeOrCopter%3F_ "plane".
- Reaction_Engines_A2 ref "Reaction engines".
- Reaction_Engines_A2 seeAlso "* Force Application and Launch from Continental United States * Supersonic transport * Reaction Engines Skylon".
- Reaction_Engines_A2 similarAircraft "* Concorde * Tupolev Tu-144".
- Reaction_Engines_A2 spanMain "41".
- Reaction_Engines_A2 status "Design study".
- Reaction_Engines_A2 type Airliner.
- Reaction_Engines_A2 type Hypersonic_speed.
- Reaction_Engines_A2 subject Category:Emerging_technologies.
- Reaction_Engines_A2 subject Category:Hydrogen-powered_aircraft.
- Reaction_Engines_A2 subject Category:Hypersonic_aircraft.
- Reaction_Engines_A2 subject Category:Proposed_aircraft_of_the_United_Kingdom.
- Reaction_Engines_A2 subject Category:Ramjet-powered_aircraft.
- Reaction_Engines_A2 subject Category:Reaction_Engines_aircraft.
- Reaction_Engines_A2 subject Category:Supersonic_transports.
- Reaction_Engines_A2 type Aircraft.
- Reaction_Engines_A2 type MeanOfTransportation.
- Reaction_Engines_A2 type Product.
- Reaction_Engines_A2 type Model_airplane.
- Reaction_Engines_A2 type DesignedArtifact.
- Reaction_Engines_A2 comment "The Reaction Engines Limited A2 (called the A2) is a design study for a hypersonic airliner intended to provide environmentally friendly, long range, high capacity commercial transportation. The aircraft is being examined as part of the LAPCAT programme of the European Union, but has not yet been commercially launched, though the British design firm Reaction Engines Limited says it could be developed into a working aircraft within 25 years once there is market demand for it.".
- Reaction_Engines_A2 label "Reaction Engines A2".
- Reaction_Engines_A2 label "Reaction Engines A2".
- Reaction_Engines_A2 label "Reaction Engines A2".
- Reaction_Engines_A2 label "Reaction Engines A2".
- Reaction_Engines_A2 label "Reaction Engines A2".
- Reaction_Engines_A2 sameAs Reaction_Engines_A2.
- Reaction_Engines_A2 sameAs Reaction_Engines_A2.
- Reaction_Engines_A2 sameAs Reaction_Engines_A2.
- Reaction_Engines_A2 sameAs Reaction_Engines_A2.
- Reaction_Engines_A2 sameAs Reaction_Engines_A2.
- Reaction_Engines_A2 sameAs m.03mhh2j.
- Reaction_Engines_A2 sameAs Q1188753.
- Reaction_Engines_A2 sameAs Q1188753.
- Reaction_Engines_A2 wasDerivedFrom Reaction_Engines_A2?oldid=602014516.
- Reaction_Engines_A2 isPrimaryTopicOf Reaction_Engines_A2.