FIELD: rocketry. SUBSTANCE: method is based on simultaneous supply of hydrogen and propellant components in form of circular jets of generator reducing gas around jets of oxygen into near-wall area of chamber. Hydrogen is fed opposite each jet of oxygen in parallel with it at velocity exceeding or equal to velocity of circular jet of generator gas, jet of oxygen and flow rate of hydrogen. EFFECT: enhanced efficiency. 7 dwg
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Authors
Dates
1997-07-10—Published
1986-09-15—Filed