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- Armstrong_Siddeley_Snarler abstract "The Armstrong Siddeley ASSn. Snarler was a small rocket engine used for mixed-power experiments with an early turbojet engine and was the first British liquid-fuelled rocket engine to fly Unlike other British rocket engine projects that used hydrogen peroxide as an oxidiser, Armstrong Siddeley's used liquid oxygen. The rocket engine is described as having a dry weight of 215 lbf (960 N) thrust of 2,000 lbf (8.9 kN) and a specific fuel consumption of 20 (lb/h)/lbf thrust. Work began in 1947 and the final configuration was first tested on 29 March 1950.The prototype of the Hawker P.1040 Sea Hawk, VP 401, had a Snarler rocket of 2,000 lbf thrust added in its tail. The Rolls-Royce Nene turbojet, of 5,200 lbf thrust, had a split tailpipe which exhausted either side of the fuselage. The combination was termed the Hawker P.1072. This gave approximately 50% greater thrust, although with twenty times the fuel consumption. It was first used in flight on 20 November 1950, by Hawker's test pilot Trevor \"Wimpy\" Wade. Half a dozen flights were made using the rocket motor before a minor explosion damaged the aircraft. Although methanol was used in the P.1072, jet fuel could be used for the Snarler. It was decided that reheat was a more practical proposition for boosting jet thrust than rockets.An unusual feature of the engine was that the turbopump was externally driven, by a drive from the gearbox of the P.1072's turbojet engine. This feature continued into the first versions of the subsequent Screamer engine, but was later replaced with a turbine-driven turbopump.".
- Armstrong_Siddeley_Snarler wikiPageID "16981570".
- Armstrong_Siddeley_Snarler wikiPageLength "5635".
- Armstrong_Siddeley_Snarler wikiPageOutDegree "24".
- Armstrong_Siddeley_Snarler wikiPageRevisionID "705761176".
- Armstrong_Siddeley_Snarler wikiPageWikiLink Afterburner.
- Armstrong_Siddeley_Snarler wikiPageWikiLink Armstrong_Siddeley.
- Armstrong_Siddeley_Snarler wikiPageWikiLink Armstrong_Siddeley_Screamer.
- Armstrong_Siddeley_Snarler wikiPageWikiLink Category:Aircraft_rocket_engines.
- Armstrong_Siddeley_Snarler wikiPageWikiLink Category:Armstrong_Siddeley_aircraft_engines.
- Armstrong_Siddeley_Snarler wikiPageWikiLink Category:Armstrong_Siddeley_rocket_engines.
- Armstrong_Siddeley_Snarler wikiPageWikiLink File:P1072.jpg.
- Armstrong_Siddeley_Snarler wikiPageWikiLink Hawker_P.1072.
- Armstrong_Siddeley_Snarler wikiPageWikiLink Hawker_Sea_Hawk.
- Armstrong_Siddeley_Snarler wikiPageWikiLink High-test_peroxide.
- Armstrong_Siddeley_Snarler wikiPageWikiLink Liquid_oxygen.
- Armstrong_Siddeley_Snarler wikiPageWikiLink Methanol.
- Armstrong_Siddeley_Snarler wikiPageWikiLink Ministry_of_Supply.
- Armstrong_Siddeley_Snarler wikiPageWikiLink Mixed-power_aircraft.
- Armstrong_Siddeley_Snarler wikiPageWikiLink Oxidizing_agent.
- Armstrong_Siddeley_Snarler wikiPageWikiLink Pound_(force).
- Armstrong_Siddeley_Snarler wikiPageWikiLink Rolls-Royce_Nene.
- Armstrong_Siddeley_Snarler wikiPageWikiLink Test_pilot.
- Armstrong_Siddeley_Snarler wikiPageWikiLink Thrust_specific_fuel_consumption.
- Armstrong_Siddeley_Snarler wikiPageWikiLink Trevor_Sidney_Wade.
- Armstrong_Siddeley_Snarler wikiPageWikiLinkText "Armstrong Siddeley Snarler".
- Armstrong_Siddeley_Snarler wikiPageWikiLinkText "Snarler".
- Armstrong_Siddeley_Snarler capacity "LOX ,".
- Armstrong_Siddeley_Snarler capacity "water-methanol".
- Armstrong_Siddeley_Snarler countryOfOrigin "United Kingdom".
- Armstrong_Siddeley_Snarler fuel "methanol/water".
- Armstrong_Siddeley_Snarler manufacturer Armstrong_Siddeley.
- Armstrong_Siddeley_Snarler name "ASSn.1 Snarler".
- Armstrong_Siddeley_Snarler oxidiser "Liquid oxygen".
- Armstrong_Siddeley_Snarler pumps "Centrifugal, mechanically driven by external shaft drive from other engine.".
- Armstrong_Siddeley_Snarler thrust "2000".
- Armstrong_Siddeley_Snarler type "liquid".
- Armstrong_Siddeley_Snarler wikiPageUsesTemplate Template:ASaeroengines.
- Armstrong_Siddeley_Snarler wikiPageUsesTemplate Template:Aviation_rocket_engines.
- Armstrong_Siddeley_Snarler wikiPageUsesTemplate Template:Convert.
- Armstrong_Siddeley_Snarler wikiPageUsesTemplate Template:Infobox_rocket_engine.
- Armstrong_Siddeley_Snarler wikiPageUsesTemplate Template:Reflist.
- Armstrong_Siddeley_Snarler subject Category:Aircraft_rocket_engines.
- Armstrong_Siddeley_Snarler subject Category:Armstrong_Siddeley_aircraft_engines.
- Armstrong_Siddeley_Snarler subject Category:Armstrong_Siddeley_rocket_engines.
- Armstrong_Siddeley_Snarler comment "The Armstrong Siddeley ASSn. Snarler was a small rocket engine used for mixed-power experiments with an early turbojet engine and was the first British liquid-fuelled rocket engine to fly Unlike other British rocket engine projects that used hydrogen peroxide as an oxidiser, Armstrong Siddeley's used liquid oxygen. The rocket engine is described as having a dry weight of 215 lbf (960 N) thrust of 2,000 lbf (8.9 kN) and a specific fuel consumption of 20 (lb/h)/lbf thrust.".
- Armstrong_Siddeley_Snarler label "Armstrong Siddeley Snarler".
- Armstrong_Siddeley_Snarler sameAs Q4793989.
- Armstrong_Siddeley_Snarler sameAs Armstrong_Siddeley_Snarler.
- Armstrong_Siddeley_Snarler sameAs アームストロング・シドレー_スナーラー.
- Armstrong_Siddeley_Snarler sameAs m.0414bzr.
- Armstrong_Siddeley_Snarler sameAs Q4793989.
- Armstrong_Siddeley_Snarler wasDerivedFrom Armstrong_Siddeley_Snarler?oldid=705761176.
- Armstrong_Siddeley_Snarler isPrimaryTopicOf Armstrong_Siddeley_Snarler.