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- Armstrong_Siddeley_Beta abstract "Armstrong Siddeley Beta was an early rocket engine, intended for use in supersonic aircraft.The Miles M.52, the intended British contender for supersonic flight, had been cancelled in 1946 due to uncertainty concerning its turbojet engine's thrust potential and the risks of manned supersonic flight. A scale model was then built by Vickers with a 362 kg (800 lbf) thrust hydrogen peroxide 'hot' motor evolved at Westcott derived from the Walter HWK 109-509 engine. This initiated the Beta and the subsequent Delta engines. In October 1948 the Vickers Transonic model flew at 930 mph (Mach 1.5) in level flight at 35,000 ft.To reduce the risks of single-sourced engines, other makers were given experience of work with hydrogen peroxide. In 1952 Napier were providing their NRE.17 engines for missile trials, as a line of development from Beta.".
- Armstrong_Siddeley_Beta wikiPageID "16985392".
- Armstrong_Siddeley_Beta wikiPageLength "2342".
- Armstrong_Siddeley_Beta wikiPageOutDegree "20".
- Armstrong_Siddeley_Beta wikiPageRevisionID "668347870".
- Armstrong_Siddeley_Beta wikiPageWikiLink Armstrong_Siddeley.
- Armstrong_Siddeley_Beta wikiPageWikiLink Armstrong_Siddeley_Delta.
- Armstrong_Siddeley_Beta wikiPageWikiLink C-Stoff.
- Armstrong_Siddeley_Beta wikiPageWikiLink C-fuel.
- Armstrong_Siddeley_Beta wikiPageWikiLink Category:Aircraft_rocket_engines.
- Armstrong_Siddeley_Beta wikiPageWikiLink Category:Armstrong_Siddeley_aircraft_engines.
- Armstrong_Siddeley_Beta wikiPageWikiLink Category:Armstrong_Siddeley_rocket_engines.
- Armstrong_Siddeley_Beta wikiPageWikiLink Category:High-test_peroxide.
- Armstrong_Siddeley_Beta wikiPageWikiLink High-test_peroxide.
- Armstrong_Siddeley_Beta wikiPageWikiLink High_test_peroxide.
- Armstrong_Siddeley_Beta wikiPageWikiLink Hydrazine.
- Armstrong_Siddeley_Beta wikiPageWikiLink Hydrogen_peroxide.
- Armstrong_Siddeley_Beta wikiPageWikiLink Methanol.
- Armstrong_Siddeley_Beta wikiPageWikiLink Miles_M.52.
- Armstrong_Siddeley_Beta wikiPageWikiLink Napier_&_Son.
- Armstrong_Siddeley_Beta wikiPageWikiLink Napier_NRE.17.
- Armstrong_Siddeley_Beta wikiPageWikiLink Rocket_Propulsion_Establishment.
- Armstrong_Siddeley_Beta wikiPageWikiLink Turbojet.
- Armstrong_Siddeley_Beta wikiPageWikiLink Vickers-Armstrongs.
- Armstrong_Siddeley_Beta wikiPageWikiLink Vickers_Armstrong.
- Armstrong_Siddeley_Beta wikiPageWikiLink Walter_HWK_109-509.
- Armstrong_Siddeley_Beta wikiPageWikiLinkText "Armstrong Siddeley Beta".
- Armstrong_Siddeley_Beta combustionChamber "Double".
- Armstrong_Siddeley_Beta countryOfOrigin "Britain".
- Armstrong_Siddeley_Beta fuel "C-fuel".
- Armstrong_Siddeley_Beta hasPhotoCollection Armstrong_Siddeley_Beta.
- Armstrong_Siddeley_Beta manufacturer Armstrong_Siddeley.
- Armstrong_Siddeley_Beta name "Beta".
- Armstrong_Siddeley_Beta oxidiser High-test_peroxide.
- Armstrong_Siddeley_Beta oxidiser High_test_peroxide.
- Armstrong_Siddeley_Beta oxidiser Hydrogen_peroxide.
- Armstrong_Siddeley_Beta pumps "First British rocket with gas-generator powered turbo-pump.".
- Armstrong_Siddeley_Beta type "liquid".
- Armstrong_Siddeley_Beta wikiPageUsesTemplate Template:ASaeroengines.
- Armstrong_Siddeley_Beta wikiPageUsesTemplate Template:Engine-aircraft-stub.
- Armstrong_Siddeley_Beta wikiPageUsesTemplate Template:Infobox_rocket_engine.
- Armstrong_Siddeley_Beta wikiPageUsesTemplate Template:Reflist.
- Armstrong_Siddeley_Beta wikiPageUsesTemplate Template:Rocket-stub.
- Armstrong_Siddeley_Beta subject Category:Aircraft_rocket_engines.
- Armstrong_Siddeley_Beta subject Category:Armstrong_Siddeley_aircraft_engines.
- Armstrong_Siddeley_Beta subject Category:Armstrong_Siddeley_rocket_engines.
- Armstrong_Siddeley_Beta subject Category:High-test_peroxide.
- Armstrong_Siddeley_Beta hypernym Engine.
- Armstrong_Siddeley_Beta type Software.
- Armstrong_Siddeley_Beta comment "Armstrong Siddeley Beta was an early rocket engine, intended for use in supersonic aircraft.The Miles M.52, the intended British contender for supersonic flight, had been cancelled in 1946 due to uncertainty concerning its turbojet engine's thrust potential and the risks of manned supersonic flight. A scale model was then built by Vickers with a 362 kg (800 lbf) thrust hydrogen peroxide 'hot' motor evolved at Westcott derived from the Walter HWK 109-509 engine.".
- Armstrong_Siddeley_Beta label "Armstrong Siddeley Beta".
- Armstrong_Siddeley_Beta sameAs m.0414jv1.
- Armstrong_Siddeley_Beta sameAs Q4793965.
- Armstrong_Siddeley_Beta sameAs Q4793965.
- Armstrong_Siddeley_Beta wasDerivedFrom Armstrong_Siddeley_Beta?oldid=668347870.
- Armstrong_Siddeley_Beta isPrimaryTopicOf Armstrong_Siddeley_Beta.