FIELD: rocketry. SUBSTANCE: in orbital injection system, using a silo with a piston separating the ballistic part with the injected object and engine from the space accommodating the launching power source for the initial acceleration of the ballistic part, the ballistic part engine is made in the form of thermonuclear charges of successive action, and the piston - in the form of a solid - reactant gas generator; the space of the launching power source has a spherical shape, and the launching power source is a chemical charge placed in vessels. EFFECT: improved design. 3 cl, 3 dwg
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