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Application filed by Havilland Engine Company LimitfiledCriticalHavilland Engine Company Limit
Publication of CH342416ApublicationCriticalpatent/CH342416A/fr
F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
F02K—JET-PROPULSION PLANTS
F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
F02K9/60—Constructional parts; Details not otherwise provided for
F02K9/68—Decomposition chambers
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Engineering & Computer Science
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Chemical & Material Sciences
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Combustion & Propulsion
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Mechanical Engineering
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General Engineering & Computer Science
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Hydrogen, Water And Hydrids
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CH342416D1959-11-151956-07-17Procédé de fonctionnement d'une installation de propulsion à fusée et installation pour la mise en oeuvre de ce procédé
CH342416A
(fr)