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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 wikiPageRevisionID "571297790".
- 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 Hydrogen_peroxide.
- Armstrong_Siddeley_Beta pumps "First British rocket with gas-generator powered turbo-pump.".
- Armstrong_Siddeley_Beta type "liquid".
- 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 type AircraftEngine102687423.
- Armstrong_Siddeley_Beta type AircraftRocketEngines.
- Armstrong_Siddeley_Beta type ArmstrongSiddeleyAircraftEngines.
- Armstrong_Siddeley_Beta type ArmstrongSiddeleyRocketEngines.
- Armstrong_Siddeley_Beta type Artifact100021939.
- Armstrong_Siddeley_Beta type Device103183080.
- Armstrong_Siddeley_Beta type Engine103287733.
- Armstrong_Siddeley_Beta type Instrumentality103575240.
- Armstrong_Siddeley_Beta type JetEngine103596285.
- Armstrong_Siddeley_Beta type Machine103699975.
- Armstrong_Siddeley_Beta type Motor103789946.
- Armstrong_Siddeley_Beta type Object100002684.
- Armstrong_Siddeley_Beta type PhysicalEntity100001930.
- Armstrong_Siddeley_Beta type Reaction-propulsionEngine104057435.
- Armstrong_Siddeley_Beta type Rocket104099175.
- Armstrong_Siddeley_Beta type Whole100003553.
- 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 sameAs Armstrong_Siddeley_Beta.
- Armstrong_Siddeley_Beta wasDerivedFrom Armstrong_Siddeley_Beta?oldid=571297790.
- Armstrong_Siddeley_Beta isPrimaryTopicOf Armstrong_Siddeley_Beta.