2012•Engineering Journal Science and InnovationRequires access

Characteristic Pilot Study of a Blended Fuel Ignition Gas-Dynamic System as Applied to Liquid-Propellant Rocket Thrusters

МГТУ им. Н.Э. Баумана, А.В. Воронецкий, К.Ю. Арефьев, МГТУ им. Н.Э. Баумана, М.А. Ильченко, ФГУП ЦИАМ им. П.И. Баранова

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Key concepts: Propellant, Liquid-propellant rocket, Rocket propellant, Ignition system, Aerospace engineering, Liquid oxygen, Rocket (weapon), Nuclear engineering